Citation
Analysis of self-propelled maintenance cart

Material Information

Title:
Analysis of self-propelled maintenance cart
Creator:
Kacena, Petr
Publication Date:
Language:
English
Physical Description:
viii, 235 leaves : illustrations, plans (6 folded in pocket) ; 29 cm

Subjects

Subjects / Keywords:
Carriages and carts -- Design and construction ( lcsh )
Maintenance -- Equipment and supplies -- Design and construction ( lcsh )
Genre:
bibliography ( marcgt )
theses ( marcgt )
non-fiction ( marcgt )

Notes

Bibliography:
Includes bibliographical references.
General Note:
Submitted in partial fulfillment of the requirements for the degree, Master of Science, Department of Mechanical Engineering
Statement of Responsibility:
by Petr Kacena.

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Source Institution:
University of Colorado Denver
Holding Location:
Auraria Library
Rights Management:
All applicable rights reserved by the source institution and holding location.
Resource Identifier:
28175835 ( OCLC )
ocm28175835

Full Text
ANALYSIS OF SELF-PROPELLED MAINTENANCE CART
by
Petr Kacena
B.S.M.E., The Czech Institute of Technology, 1987
A thesis submitted to the
Faculty of the Graduate School of the
University of Colorado at Denver
in partial fulfillment
of the requirements for the degree of
Master of Science
Mechanical Engineering


This thesis for the Master of Science
degree by
Petr Kacena
has been approved for the
Department of
Mechanical Engineering
by
James C. Gerdeen
Date


Petr Kacena (M.S., Mechanical Engineering)
Analysis of Selfpropelled Maintenance Cart
Thesis directed by Assistant Professor Rafael L. Sanchez
ABSTRACT
The prime objective of this thesis is to perform analysis
of a selfpropelled maintenance cart, travelling on an
elevated conveyor structure. The cart is a frame
structure with one top platform and one left and right
removable side cage. The main purpose of the cart is to
provide maintenance and inspection access to the conveyor
componentry. The maintenance cart is propelled by two
chain drive units. These units consist of electrical
motor, reducer, clutch brake, and two horizontal friction
drive wheels. The drive units are located at the front
and back of the cart. The friction drive wheels are on
the centerline of the cart and are in permanent contact
with the guiding tee section, which is welded on the top
of trusses.
iii


The cart has to operate under any weather condition and
must meet all safety requirements. To accomplish the
above, the following analysis will be performed:
- deformation and stress analysis
- propel system analysis
- vibration analysis.
The stress and deflection analysis of a maintenance cart
structure under different load modes is done by using the
finite element method. The commercial package STAAD-III
release 15 has been used for the FEA modeling,
preprocessing, and postprocessing. To achieve a uniform
reliability for the cart structural members under various
loading conditions, the loads are specified in accordance
with the Load and Resistance Factor Design (LRFD)
specification instead of the more traditional Allowable
Stress Design (ASD) method.
This abstract accurately represents the content of the
candidate's thesis. I recommend its publication.
Signed
Rafael L. Sanchez
iv


CONTENTS
Symbols and Abbreviations..............................vii
1. Objective............................................1
1.1 Introduction.........................................1
1.2 Deformation and Stress Analysis......................2
1.3 Propel System Analysis...............................3
1.4 Vibration Analysis...................................3
2. General System Description...........................4
2.1 Location.............................................4
2.2 Climate..............................................4
2.3 Conveyor Description.................................4
2.4 Maintenance Carriage.................................5
3. FEA Analysis of the Maintenance Cart.................7
3.1 Introduction to STAAD-III............................7
3.2 FEA Model of Maintenance Cart........................9
3.3 Loads...............................................11
3.3.1 Dead Loads........................................11
3.3. l.l Machinery......................................12
3.3.1.2 Power Generator................................13
3.3.1.3 Thruster.......................................13
3.3.1.4 Motor Control Center...........................14
v


3.3.1.5 Checker Plate...................................14
3.3.1.6 Self-Weight of the Maintenance Cart.............15
3.3.2 Live Loads........................................15
3.3.3 Wind Loads........................................16
3.3.3.1 Operating Wind..................................16
3.3.3.2 Storm Wind......................................17
3.3.4 Snow Load.........................................18
3.3.5 Temperature Load..................................19
3.4 Load Combinations...................................20
3.5 Results of the FEA analysis.........................22
3.6 Interpretation of Results..........................203
3.6.1 Support Reactions................................203
3.6.2 Joint Displacement...............................204
3.6.3 Member Forces and Stresses......................2 05
3.6.4 Member Sizes.....................................207
4. Propel System Analysis.............................212
5. Vibration Analysis.................................217
5.1 Undamped Free Vibrations...........................219
6. Bibliography.......................................235
vi


SYMBOLS AND ABBREVIATIONS
A area
d diameter
F force
ft foot or feet
ft-lb foot-pound
g gravitational acceleration constant
hp horsepower
i radius of gyration
in inch
in-lb inch-lb
J moment of inertia
K spring constant
1 or L length
lb pound
m mass
n cycles
P pressure pre unit area
psf pounds per square foot
psi pounds per square inch
Q force
Vll


q load per unit length
R radius, radius of gyration
rad radian
rpm revolutions per minute
rps revolutions per second
T torque
V velocity
W weight, total load
w load per unit length
X, y, z coordinates
5 deflection
e tensile or compressive strain
Poisson's ratio
a normal stress
T shearing stress
ur angular velocity
>
viii


1. Objective
1.1 Introduction
The prime objective of this thesis is to perform
analysis of a selfpropelled maintenance cart travelling on
an elevated conveyor structure. The conveyor system,
located at Eccles Canyon Area in Utah, transports crushed
coal from an underground mine to the rail loadout facility.
The system originates at a surface crusher building at
elevation 8600 feet and terminates by feeding an inclined
conveyor at elevation 8000 feet. The overall conveying
length is 11,200 feet with elevation drop 600 feet. The
conveyor is an elevated structure made of 60 feet long
truss sections and the head end consists of 120 feet long
galleries. The conveyor follows a path generally parallel
to a adjacent highway. Thus the conveyor route is a
combination of straight sections and sections with
horizontal, vertical and combined curves. The maximum
angle between two adjacent trusses is 3.
To provide a maintenance and inspection access, a
self- propelled maintenance cart was design to travel about
10,500 feet on the elevated trusses. The cart is a frame
1


structure with one top platform and one left and right
removable side cage. The main purpose of the side cages is
to provide access to the conveyor componentry. The
maintenance cart is propelled by two chain drive units.
These units consists of electrical motor, reducer, clutch
brake, and two horizontal friction drive wheels. The drive
units are located at the front and back of the cart. The
friction drive wheels are on the centerline of the cart and
are in permanent contact with the guiding tee section,
which is welded on the top of trusses.
The cart has to operate under any weather condition and
must meet all safety requirements. To accomplish the
above, the following analysis will be performed:
- deformation and stress analysis
- propel system analysis
- vibration analysis.
1.2 Deformation and Stress Analysis
The stress and deflection analysis of a maintenance
cart structure under different load modes is done by using
the finite element method. I used the commercial package
STAAD-III release 16 for the FEA modeling, preprocessing,
and postprocessing. To achieve a uniform reliability for
2


the cart structural members under various loading
conditions, the loads are specified in accordance with the
Load and Resistance Factor Design (LRFD) specification
instead of the more traditional Allowable Stress Design
(ASD) method. Load and Resistance Factor Design method
uses separate factors for each load and resistance.
Because the different factors reflect the degree of
uncertainty of different loads and combinations of loads
and of the accuracy of predicted strength, a more uniform
reliability of the structure is possible.
1.3 Propel System Analysis
This stage involves analysis of the proposed "Propel
System" and calculation of starting torque, running torque
for different slopes, and calculation of maximum required
horsepower.
1.4 Vibration Analysis
The main goal is to investigate maintenance cart
behavior in curves under different ambient conditions and
to determine any possible problems.
3


2. General System Description
2.1 Location
SKYLINE MINES Utah Fuel Company, Eccles Canyon,
Area Helper, Utah.
2.2 Climate
High temperature in the summer +90 degrees F. Lows in
the winter reach -50 degrees F. Average area snowfall is
240 inches per year. The conveying route progresses
through the Eccles Canyon which is oriented in an east-west
direction. The winds blow up and down the canyon,
generally in the westerly direction. Typical velocities of
the conveyor are 3 to 7 miles per hour.
2.3 Conveyor Description
The pipe conveyor transports crushed coal from an
underground mine to the rail loadout facility. The system
4


originates at a surface crusher building at an elevation of
8600 feet and terminates by feeding an inclined conveyor at
8000 feet. The coal is then carried to the top of storage
silos. The overall conveying length is 11,200 feet with an
elevation drop of 600 feet.
The conveying system is a single flight design with no
intermediate drives or transfer station between the crusher
building and the loadout facility. To minimize the
environmental impact along the conveying route the conveyor
follows a path generally parallel to an adjacent highway
which in turn necessitates vertical, horizontal, and
compound curves.
To minimize the potential of spills and excess dust a
special type of belt is used in this application The Pipe
Belt Conveyor.
The system consists of three parts: loading station,
overland conveyor, and unloading/discharge station.
Main goals for the conveyor design are:
- to provide reliable conveyor system.
- to minimize the environmental impact during normal
operation, during inspection, servicing, and
maintenance, and during potential failure modes.
- to minimize the potential for casual access.
- to provide crossing for small animals and deer along
the entire conveyor length.
5


2.4 Maintenance Carriage
A self-propelled maintenance carriage was designed to
travel about 10,500 feet on the elevated conveyor structure
and to allow access to all belt conveyor components for
inspection and maintenance. The elevated conveyor
structure consists of 173 trusses each 60 feet long.
The carriage incorporates all necessary devices,
propulsion system, and working and maintenance platforms.
Special care was taken to ensure the unit's safe operation
in all anticipated foul weather conditions.
6


3
FEA Analysis of the Maintenance Cart
3.1 Introduction to STAAD-III
STAAD-III is a fully integrated software package
capable of analysis, design, and drafting. The STAAD-III
environment can be thought of as a shell encompassing
analysis, design, graphics, and drafting modules. The
STAAD-III input file can be input either by using a
command-driven problem-oriented language (POL) or by
interface with AutoCAD and AutoSTAAD. The output results
are written to an output file. The deflected/mode shapes,
the moment/shear, and the stress diagrams can be displayed.
The stiffness analysis applied in the STAAD-III uses
the matrix displacement method. In the matrix analysis of
complex structures the structure is first discretized into
an assembly of discrete structural elements. The
displacement of each element has to satisfy the force
equilibrium and displacement compatibility at the joints;
the displacement at points inside an element need to be
represented in terms of the nodal displacements of the
element.
7


Such a discrete element analysis of structures, having
elements which are continuously attached to one another,
resolves to element forces at nodal points. This idealized
solution has no physical counterpart in the reality. These
forces must therefore, be consistent as a set of equivalent
discrete forces replacing the continuously varying stress
field. Displacements of the joints are equal to the actual
displacements of the corresponding joints on the structure.
After calculating the actual displacement, the element
forces can be easily determined.
The element forces are introduced only at nodal
points, and thus any external loading must be applied or
converted at these points as concentrated forces and
moments. The global stiffness matrix of the structure is
obtained by methodically summing the various members and
element stiffness matrixes. The external loads on the
structure are represented as discrete concentrated loads
acting only at the nodal points of the structure. The
stiffness matrix relates these loads to the displacement of
the nodes by the equation:
Aj = aj + Sj Dj (3.1)
The formulation (3.1) includes all the joints of the
structure, whether they are free to displace or are
8


restrained by supports. The components of joint
displacements that are free to move are called "degrees of
freedom". The number of unknowns in the analysis
represents the total member of degrees of freedom.
There are many methods to solve the unknowns from a
series of simultaneous equations. STAAD III implements
decomposition called "Modified Cholesky's Method". This
method is very accurate and well suited for the Gaussian
elimination process in solving the simultaneous equations.
3.2 FEA Model of the Maintenance Cart
The three dimensional wire-framed pictures of the
Maintenance cart FEA model is shown on Figure 3-1, and on
an enclosed drawing CART-3D.
The drawings CART-1R shows the right outside and front
of the maintenance cart.
The drawing CART-1L shows the left outside side and
back of the cart.
The drawing CART-3T shows the top platform, inside of
the left cage, and the drive wheel assembly arrangement.
9


.J/


The drawing CART-4T shows the top platform's inside
handrail, the inside of the right-side cage, and the drive
wheel assembly.
The FEA MODEL consists of 138 nodes and 227 elements.
The joint members 89, 90, 91, and 91 are fixed supports
with Fx, Fz, Mx, My, and Mz being released to simulate the
rolling support of vertical wheels. The horizontal drive
wheels supports are most closely modeled by fixed support
with Fy, Mx, My, and Mz being released.
The pinned support has translational, but no
rotational constraints. In other words, the support has no
moment carrying capacity.
Regarding the fixed support it has both translational
and rotational constraints, but in our case the fixed
supports have only vertical constraint since all other
constraints have been released. The connectivity from
members is described through the member incidence command.
The problem statistics are:
- Number of joints = 138
- Number of elements = 227
- Number of supports = 8
- Fixed support nodes 89, 90, 91, and 92 with Fx, Fz, Mx,
My, and Mz released
10


- Fixed supports = nodes 96, 100, 104, 108 with Fy, Mx,
My, and Mz released.
- Total primary load cases = 7
- Total degrees of freedom = 812
- Size of stiffness matrix = 103, 936 double precision
words
- Total required disk space = 14.25 Mega-bytes
The program has been run on an IBM compatible 486, 33 Mhz
computer.
3.3 Loads
The accurate determination of the loads to which a
maintenance cart is subjected is one of the first important
steps in the analysis.
There are several kinds of loads which are to be
acting on the maintenance cart. In the next section I will
investigate all which may apply.
3.3.1 Dead Loads
Dead load is a fixed position gravity service load
acting continuously towards the earth.
11


3.3. l.l Machinery
Motor
Reducer
Clutch
Sprocket
Pillow block
Disk brake
Thruster
Wl=125 lb
W2=246 lb
W3=100 lb
W4=16 lb
W5=ll lb
W6=120 lb
W7=200 lb
W8=2000 lb
Power generator
Motor control center W9=200 lb
Drive unit weight = WD
WDT = W1+W2+W3+W4+2*W5+2*W6 = 645 lb
WD = 1.1 WDT
AREA = 22*24 = 528 in2
p = wd/A = 710/528 = 1.345 lb/in2
(3.2)
(3.3)
(3.4)
(3.5)
As the calculation indicates the dead load per unit area is
1.345 lb/in. The area load (pressure) due to the dead
weight of drive unit can be specified as:
153 154 184 179 185 ALOAD 1.345
140 141 187 182 186 ALOAD 1.345
where the numbers 153, 154 and so on represent the members
over which the area load is applied.
12


3.3.1.2 Power Generator
The weight of the power generator W6 is 2000 lbs and
is acting over A2 area, where
A2 = 37.25 46.5 = 1732.125 in2 (3.6)
P = W6/A2 = 1.155 lb/in2 (3.7)
Thus the dead load per unit area due to the dead weight of
the generator is 1.155 lb/in2 and the area load due to dead
weight of the power generator can be specified as:
AREA LOAD:
197 163 164 198 174 173 ALOAD 1.155
3.3.1.3 Thruster
The dead weight of thruster WT = 2 00 lb acting over
members 160 and 170. The length of members 160 and 170 is
L=36". Then:
f = Wt/L = 200/36 = 5.56 lb/in (3.8)
where f = load per unit length and the member load due to
the dead weight of thruster can be specified as:
MEMBER LOAD:
160 170 UNI GY -5.56
13


3.3.1.4 Motor Control Center
The dead weight of the motor control center WE=200 lbs
and it is acting over members 149, 150, 168, and 169. The
best way to represent this load is as member load.
L = 41+2*24 = 89 in (3.9)
f = We/L = 2.25 lb/in (3.10)
Hence the member load:
150 168 169 UNI GY
149 UNI GY -2.25 33
-2.25
57
3.3.1.5 Checker Plate
The top platform serves as a working area for the crew
of the maintenance cart and thus the floor is made out of
3/16 checkered plate. This weight has to be included in
the analysis as dead weight.
The unit weight of 3/16 checkered plate
wcm = 8.91 lb/ft2 = 0.062 lb/in2 and thus the area load can
be specified as:
131 132 133 134 135 136 195 163 162 194 189
14


192 ALOAD
0.062
136 137 138 167 166 165 164 195 ALOAD 0.062
161 162 197 172 171 196 ALOAD - 0 . 062
146 147 148 149 150 168 169 170 171 172 173
201 191 202 ALOAD i 0 .062
12 34 10 9 8 7 6 5 ALOAD - 0.062
15 16 17 18 19 20 14 13 12 11 ALOAD 0.062
3.3.1.6 Self-Weight of the Maintenance Cart
To calculate and use self-weight of maintenance cart
in the analysis, self-weight function will be used with 1.1
factor (this provides for 10% safety factor).
Hence self-weight Y = -1.1.
3.3.2 Live Loads
All gravity loads acting when the structure is in
service, but varying in magnitude and location, will be
termed live loads. Because of the unknown nature of the
15


magnitude, location, and density of live load items,
realistic magnitudes and positions of such loads are very
difficult to determine. The best way to represent this
load is as a JOINT LOAD. In this study the live loads are
considered to be egual to the average weight of two
maintenance crew members. Since the location of live loads
vary they will be allocated in the location which will
cause most adverse effect on the stability and deflection
of the cart. Thus if a wind load is assumed from the
right side the live load can be specified as:
JOINT LOAD:
2 3 FY 250.0
3.3.3 Wind Load
3.3.3.l Operating Wind
The maintenance cart is moving on an elevated conveyor
structure and thus wind loads must be considered in the
analysis.
16


q = 5 psf
(3.11)
P = cf * q = 2.5 = 10 psf = 0.0694 lb/in (3.12)
and the wind load can be represented by uniform area load
of magnitude 0.0694 lb/in2, where
A = 138 * 100 = 13800 in2 (3.13)
F = p * A =13800 0.0694 = 958 lb (3.14)
In the analysis the wind load is acting from the right side
to the left and must be taken by members of the right cage
and then the main members subjected to this load are: 16,
17, 18, 19, 70, 71, 72, 145, 146, 147, 148, 149, 69, 68,
and 67, which total length L =2(138+100)=476 in.
f= F/L = 958/476 =2.01 lb/in (3.15)
Hence the operation wind load can be represented as a
MEMBER LOAD:
16 17 18 19 70 71 72 145
149 69 68 67 UNI GZ -2.01
147
148
3.3.3.2 Storm Wind
v=7 0 mph, EXPOSURE B
Average height = O'- 20', cE=0.7
17


q = 0.7 1.0 13 = 9.1 psf
(3.16)
Cf = 2
(3.17)
p = cf*q = 2 9.1 = 18.2 psf = 0.12 64 lb/in2
(3.18)
A = 13800 in2
(3.19)
F = p A = 0.1264 13800 = 1744.2 lb
(3.20)
f = F/L where L = 476 in
f = 1744.2/476 = 3.66 lb/in
(3.22)
(3.21)
Thus the storm wind can be specified as member load:
MEMBER LOAD:
16 17 18 19 70 71 72 145 146 147 148
149 69 68 67 UNI GZ -3.66
i
3.3.4 Snow Load
The best procedure for establishing the snow load is
to follow the ANSI standard. This code uses a map of the
United States giving isolines of ground snow corresponding
to a 50 year mean recurrence interval. In our case the
snow load per unit area is 0.365 lb/in2. Hence to represent
snow load the AREA LOAD specification will be used.
18


AREA LOAD:
131 132 133 134 135 195 163 162 194 189 192
ALOAD-O.365
136 137 138 167 166 165 164 195 ALOAD-0.365
161 162 197 172 171 196 ALOAD-0.365
146 147 148 149 150 168 169 170 171 172 173 201
191 202 ALOAD -0. 365
3.3.5 Temperature Load
The maintenance cart structure is a rigid welded
structure, thus the effect of temperature changes needs to
be considered. High temperature in the summer is 90 F and
low in the winter is -50 F. Thus if the mean temperature
is taken (50 degrees F), then the maximum difference is -
100 F and the temperature load will effect all 277 members.
Thus we have:
TEMPERATURE LOAD (WINTER)
1 to 277 TEMP -100
TEMPERATURE LOAD (SUMMER)
1 to 277 TEMP 50.0
19


3.4 Load Combinations
The required strength of the structure and its
elements must be determined from an appropriate critical
combination of factored loads. The most critical effect
may be when one or more loads are not acting. The
probability-based load criteria are represented in the ANSI
factored load combinations. The LRFD-A 4.1 specifies that
the following combinations shall be investigated:
1. 1.4 D (3.23)
2. 1.2 D + 1.6 L + 0.5 (Lr or S or R) (3.24)
3. 1.2 D + 1.6 (Lr or S or R) + (0.5 L or 0.8 W) (3.25)
4. 1.2 D + 1.3 W + 0.5 L + 0.5 (Lr or S or R) (3.26)
5. 1.2 D + 1.5 E + (0.5 L + 0.2 S) (3.27)
6. 0.9 D - (1.3 W or 1.5 E) (3.28)
Where the nominal service loads are:
D = dead load
L = live load
W = wind load
S = snow load
E = earthquake load
Lr = roof live load
20


R = rain water or ice loads
Note that D, L, W, S, etc. are loads in general sense,
which includes bending moment, shear, axial force, and
torsional moment.
In the analysis, load combinations 100, 110, 120, 130, and
140 were used.
Load Combination 100:
1.4 D
The load due to dead weight is prevailing.
Load Combination 110;
1.2 D + 1.6 L + 0.5 W
This combination represents the load on maintenance cart
under normal operating conditions.
Load Combination 120:
1.2 D + 0.5 L + 1.3 W
This combination represents the load on maintenance cart
under storm wind condition.
Load Combination 130:
1.2 D + 0.5 L + 1.6 S + 1.0 T
This represents the loads on maintenance cart under winter
conditions, i.e. the snow and the temperature changes are
21


important factors.
Load Combination 140;
1.2 D + 0.5 L + 0.5 S + 1.3 W + 1.0 T
The load combination 140 represents the winter storm
condition.
3.5 Results of FEA Analysis
The next section contains the printouts of the FEA
analysis. As specified in section 3.4, the behavior of the
maintenance cart was investigated under different load
combinations.
Pages no. 36 to 38 give support reactions for each
load combination.
Pages no. 39 to 57 show the joint displacement for
appropriate load combination.
Pages 58 to 118 give the member forces. The results
for stresses are on pages 119 to 173.
To check if the sizes of members are sufficient, the
code checking function was used. The results are on pages
174 to 187.
The pages 190 to 201 show suggested member sizes.
22


*
*
* STAAD-III *
* REVISION 15.0 (VERSION 15 LEVEL 0) *
* PROPRIETARY PROGRAM OF *
* RESEARCH ENGINEERS,INC. *
* DATE= DEC 1, 1992 *
* TIME= 21:46:14 *
* *
**************************************************
1. STAAD SPACE
3. *** MAINTENANCE CART STRESS & DEFLECTION ANALYSIS ***
4. *** NAME: PETR KACENA ***
6. *
7. PAGE LENGTH 55
8. *
9. UNIT POUND INCH
10. *
11. OUTPUT WIDTH 55
12. *
13. JOINT COORD
14. 1 0.0 0.0 0.0
15. 2 47.0 0.0 0.0
16. 3 69.0 0.0 0.0
17. 4 94.0 0.0 0.0
18. 5 138.0 0.0 0.0
19. 6 0.0 0.0 32.0
20. 7 47.0 0.0 32.0
21. 8 69.0 0.0 32.0
22. 9 94.0 0.0 32.0
23. 10 138.0 0.0 32.0
24. 11 0.0 0.0 96.5
25. 12 44.0 0.0 96.5
26. 13 69.0 0.0 96.5
27. 14 91.0 0.0 96.5
28. 15 138.0 0.0 96.5
29. 16 0.0 0.0 128.5
30. 17 44.0 0.0 128.5
31. 18 69.0 0.0 128.5
32. 19 91.0 0.0 128.5
33. 20 138.0 0.0 128.5
34. 21 0.0 36.0 0.0
35. 22 69.0 36.0 0.0
36. 23 138.0 36.0 0.0
37. 24 0.0 36.0 32.0
23


STAAD SPACE
38. 25 47.( 3 36.0 32.0
39. 26 94.( 3 36.0 32.0
40. 27 138, .0 36. 0 32.0
41. 28 0.0 36.0 96.5
42. 29 44.( 3 36.0 96.5
43. 30 91.( 3 36.0 96.5
44. 31 138, .0 36. 0 96.5
45. 32 0.0 36.0 128.5
46. 33 69.( 3 36.0 128.5
47. 34 138, .0 36. 0 128.5
48. 35 0.0 84.0 0.0
49. 36 138, ,0 84. 0 0.0
50. 37 0.0 84.0 32.0
51. 38 138, ,0 84. 0 32.0
52. 39 0.0 84.0 96.5
53. 40 138, ,0 84. 0 96.5
54. 41 0.0 84.0 128.5
55. 42 138, ,0 84. 0 128.5
56. 43 0.0 100.0 0.0
57. 44 32.1 5 100. 0 0.0
58. 45 49.C ) 100. 0 0.0
59. 46 60.( ) 100. 0 0.0
60. 47 69.C ) 100. 0 0.0
61. 48 78.C ) 100. 0 0.0
62. 49 106. ,0 100 .0 0.0
63. 50 138, ,0 100 .0 0.0
64. 51 138. ,0 100 .0 32.0
65. 52 138. ,0 100 .0 41.0
66. 53 138. ,0 100 .0 53.25
67. 54 138. ,0 100 .0 64.25
68. 55 138. ,0 100 .0 75.25
69. 56 138. ,0 100 .0 87.5
70. 57 138. ,0 100 .0 96.5
71. 58 138. 0 100 .0 128.5
72. 59 105. 5 100 .0 128.5
73. 60 89. C ) 100. 0 128.5
74. 61 69.C ) 100. 0 128.5
75. 62 57.C ) 100. 0 128.5
76. 63 0.0 100.0 128.5
77. 64 0.0 100.0 96.5
78. 65 0.0 100.0 87.5
79. 66 0.0 100.0 75.25
80. 67 0.0 100.0 64.25
81. 68 0.0 100.0 53.25
82. 69 0.0 100.0 41.0
83. 70 0.0 100.0 32.0
84. 71 24.C ) 100. 0 41.0
85. 72 42.C ) 100. 0 41.0
86. 73 49.C ) 100. 0 41.0
24


STAAD SPACE
*****************************************************
87. 74 70.75 100.0 41.0
88. 75 106.0 100.0 41.0
89. 76 108.0 100.0 41.0
90. 77 114.0 100.0 41.0
91. 78 24.0 100.0 87.5
92. 79 42.0 100.0 87.5
93. 80 57.0 100.0 87.5
94. 81 70.75 100.0 87.5
95. 82 89.0 100.0 87.5
96. 83 108.0 100.0 87.5
97. 84 114.0 100.0 87.5
98. 85 32.5 100.0 32.0
99. 86 49.0 100.0 32.0
100. 87 105.5 100.0 96.5
101. 88 89.0 100.0 96.5
102. 89 14.0 100.0 41.0
103. 90 124.0 100.0 41.0
104. 91 14.0 100.0 87.5
105. 92 124.0 100.0 87.5
106. 93 0.0 88.0 75.25
107. 94 0.0 88.0 53.25
108. 95 14.0 88.0 53.25
109. 96 14.0 88.0 64.2
110. 97 24.0 88.0 53.25
111. 98 24.0 88.0 75.25
112. 99 14.0 88.0 75.25
113. 100 14.0 88.0 64.3
114. 101 114.0 88.0 75.25
115. 102 114.0 88.0 53.25
116. 103 124.0 88.0 53.25
117. 104 124.0 88.0 64.2
118. 105 138.0 88.0 53.25
119. 106 138.0 88.0 75.25
120. 107 124.0 88.0 75.25
121. 108 124.0 88.0 64.3
122. 109 0.0 124.75 0.0
123. 110 49.0 124.75 0.0
124. 111 106.0 124.75 0.0
125. 112 138.0 124.75 0.0
126. 113 138.0 124.75 128
127. 114 89.0 124.75 128.
128. 115 57.0 124.75 128.
129. 116 0.0 124.75 128.5
130. 117 0.0 142.75 0.0
131. 118 49.0 142.75 0.0
132. 119 106.0 142.75 0.0
133. 120 138.0 142.75 0.0
134. 121 138.0 142.75 32.
135. 122 138.0 142.75 96.
25


STAAD SPACE
*****************************************************
136. 123 138.0 142.75 128.5
137. 124 89.0 142.75 128.5
138. 125 57.0 142.75 128.5
139. 126 0.0 142.75 128.5
140. 127 0.0 142.75 96.5
141. 128 0.0 142.75 32.0
142. 129 32.5 142.75 32.0
143. 130 105.5 142.75 96.5
144. 131 94.0 84.0 32.0
145. 132 47.0 84.0 32.0
146. 133 44.0 84.0 96.5
147. 134 91.0 84.0 96.5
148. 135 24.0 100.0 53.25
149. 136 24.0 100.0 75.25
150. 137 114.0 100.0 53.25
151. 138 114.0 100.0 75.25
152. *
153. MEMBER INCIDENCES
154. 112
155. 223
156. 334
157. 445
158. 516
159. 667
160. 778
161. 889
162. 9 9 10
163. 10 5 10
164. 11 11 12
165. 12 12 13
166. 13 13 14
167. 14 14 15
168. 15 11 16
169. 16 16 17
170. 17 17 18
171. 18 18 19
172. 19 19 20
173. 20 15 20
174. 21 2 7
175. 22 4 9
176. 23 12 17
177. 24 14 19
178. 25 3 21
179. 26 3 22
180. 27 3 23
181. 28 21 22
182. 29 22 23
183. 30 1 21
184. 31 21 35
26


STAAD SPACE
*****************************************************
185. 32 35 43
186. 33 21 47
187. 34 23 47
188. 35 5 ; 23
189. 36 23 36
190. 37 36 50
191. 38 6 ; 24
192. 39 24 37
193. 40 37 70
194. 41 10 27
195. 42 27 38
196. 43 38 51
197. 44 7 ; 25
198. 45 25 132
199. 46 9 ; 26
200. 47 26 131
201. 48 25 26
202. 49 24 25
203. 50 38 131
204. 51 131 132
205. 52 37 132
206. 53 15 31
207. 54 31 40
208. 55 40 57
209. 56 11 28
210. 57 28 39
211. 58 39 64
212. 59 14 30
213. 60 30 134
214. 61 12 29
215. 62 29 133
216. 63 30 31
217. 64 29 30
218. 65 40 134
219. 66 133 134
220. 67 16 32
221. 68 32 41
222. 69 41 63
223. 70 20 34
224. 71 34 42
225. 72 42 58
226. 73 18 33
227. 74 32 33
228. 75 33 34
229. 76 18 32
230. 77 18 34
231. 78 34 61
232. 79 32 61
233. 80 21 24
27


STAAD SPACE
*****************************************************
234. 81 35 37
235. 82 28 32
236. 83 39 41
237. 84 23 27
238. 85 36 38
239. 86 31 34
240. 87 40 42
241. 88 43 109
242. 89 109 117
243. 90 45 110
244. 91 110 118
245. 92 49 111
246. 93 111 119
247. 94 50 112
248. 95 112 120
249. 96 109 110
250. 97 117 118
251. 98 118 119
252. 99 110 111
253. 100 120 121
254. 101 121 122
255. 102 122 123
256. 103 50 121
257. 104 54 121
258. 105 54 122
259. 106 58 122
260. 107 60 114
261. 108 114 124
262. 109 62 115
263. 110 115 125
264. 111 63 116
265. 112 116 126
266. 113 113 114
267. 114 123 124
268. 115 115 116
269. 116 125 126
270. 117 64 127
271. 118 70 128
272. 119 126 127
273. 120 127 128
274. 121 117 128
275. 122 63 127
276. 123 67 127
277. 124 67 128
278. 125 43 128
279. 126 128 129
280. 127 122 130
281. 128 129 85
282. 129 130 87
28


STAAD SPACE
******T*:r********************************************
283. 130 43 44 136
284. 137 50 51 144
285. 145 58 59 149
286. 150 63 64 156
287. 157 43 70
288. 158 69 89
289. 159 89 71
290. 160 71 72 165
291. 166 77 90
292. 167 90 52
293. 168 65 91
294. 169 91 78
295. 170 78 79 175
296 . 176 84 92
297. 177 92 56
298. 178 78 136
299. 179 136 i 135
300. 180 71 135
301. 181 84 138
302. 182 138 1 137
303. 183 77 137
304. 184 68 135
305. 185 66 136
306. 186 53 137
307. 187 55 138
308. 188 70 85
309. 189 85 86
310. 190 57 87
311. 191 87 88
312. 192 44 85
313. 193 45 86
314. 194 73 86
315. 195 49 75
316. 196 72 79
317. 197 74 81
318. 198 76 83
319. 199 62 80
320. 200 60 88
321. 201 82 88
322. 202 59 87
323. 203 93 94
324. 204 94 95
325. 205 95 97
326. 206 97 98
327. 207 98 99
328. 208 99 93
329. 209 101 . 102
330. 210 102 ! 103
331. 211 102 1 105
29


STAAD SPACE
**x*************************************************
332. 212 106 105
333. 213 106 107
334. 214 101 107
335 . 215 96 95
336. 216 99 100
337. 217 103 104
338. 218 107 108
339. 219 51 121
340. 220 57 122
341. 221 58 113
342. 222 113 123
343. 223 133 39
344. 224 66 93
345. 225 98 136
346. 226 101 138
347. 227 55 106
348. *
349. START USER TABLE
350. TABLE 1 HSSFILE
351. TABLE 2
352. UNIT INCHES
353. TUBE
354. TUB20202
355. 0.90, 2.0, 2.0, 0.125, 0.125, 0.668, 0.668,
356. END
357. *
358. MEMBER PROPERTIES
359. 1 TO 129 UPT 2 TUB20202
360. 130 TO 187 TA ST TUB30304
361. 188 TO 202 UPT 2 TUB20202
362. 203 TO 218 TA ST TUB30304
363. 219 TO 223 UPT 2 TUB20202
364. 224 TO 227 TA ST TUB30304
365. *
366. CONSTANTS
367. E STEEL ALL
368. DENSITY STEEL ALL
369. ALPHA 0.0000065
370. *
371. SUPPORTS
372. 89 90 91 92 FIXED BUT FX FZ MX MY MZ
373. 96 100 104 108 PINNED
374. *
375. LOADING 1 *** DEAD LOAD
376. SELFWEIGHT Y -1.1
377. AREA LOAD
378. *** DRIVE UNIT
379. 153 154 184 179 185 ALOAD -1.345
380. 140 141 187 182 186 ALOAD -1.345
0.846, 0.871, 0.871
30


STAAD SPACE
********************************T*******************
381. *** GENERATOR
382. 197 163 164 198 174 173 ALOAD -1.155
383. MEMBER LOAD
384. *** EL. CENTER UNIT
385. 150 168 169 UNI GY -2.25
386. 149 UNI GY -2.25 33 57
387. ***THRUSTER
388. 160 170 UNI GY -5.56
389. AREA LOAD
390. *** CHECKER PL.
391. 131 132 133 134 135 195 163 162 194 189 192 ALOAD -0.062
392. 136 137 138 167 166 165 164 195 ALOAD -0.062
393. 161 162 197 172 171 196 ALOAD -0.062
394. 146 147 148 149 150 168 169 170 171 172 173 201 191 202 ALOAD -0.062
395. 1234 10 98765 ALOAD -0.062
396. 15 16 17 18 19 20 14 13 12 11 ALOAD -0.062
397. *
398. *
399. LOADING 2 ** LIVE LOAD
400. JOINT LOAD
401. 2 3 FY -250.0
402. *
403. LOADING 3 *** OPERATING WIND 5 PSF
404. MEMBER LOAD
405. 16 17 18 19 70 71 72 145 146 147 148 149 69 68 67 UNI GZ -2.01
406. *
407. *
408. LOADING 4 *** SNOW LOAD
409. AREA LOAD
410. 131 132 133 134 135 195 163 162 194 189 192 ALOAD -0.365
411. 136 137 138 167 166 165 164 195 ALOAD -0.365
412. 161 162 197 172 171 196 ALOAD -0.365
413. 146 147 148 149 150 168 169 170 171 172 173 201 191 202 ALOAD -0.365
414. *
415. LOADING 5 *** STORM WIND
416. MEMBER LOAD
417. 16 17 18 19 70 71 72 145 146 147 148 149 69 68 67 UNI GZ -3.66
418. *
419. LOADING 6 *** TEMPERATURE LOAD WINTER
420. TEMPERATURE LOAD
421. 1 TO 227 TEMP -100.0
422. *
423. LOADING 7 *** TEMPERATURE LOAD SUMMER
424. TEMPERATURE LOAD
425. 1 TO 227 TEMP 50.0
426. *
427. LOAD COMBINATION 100 ** DEAD WEIGHT
428. 1 1.4
429. *
31


STAAD SPACE
***************************************T*************
420. LOAD COMBINATION 110 ** NORMAL CONDITIONS
431. 1 1.2 2 1.6 3 0.5
432. *
433. LOAD COMBINATION 120 ** STORM WIND
434. 1 1.2 2 0.5 5 1.3
435. *
436. LOAD COMBINATION 130 ** SNOW LOAD
437. 1 1.2 2 0.5 4 1.6 6 1.0
438. *
439. LOAD COMBINATION 140 ** WINTER STORM
440. 1 1.2 2 0.5 4 0.5 5 1.3 6 1.0
441. *
442. PAGE NEW
32


STAAD SPACE
*****************************************************
443. ******************************
444. ****PROBLEM STATISTICS********
445. ******************************
446. PRINT PROBLEM STATISTICS
PROBLEM STATISTICS
NUMBER OF JOINTS/MEMBER+ELEMENTS/SUPPORTS = 138/ 227/
ORIGINAL/FINAL BAND-WIDTH = 107/ 21
TOTAL PRIMARY LOAD CASES = 7, TOTAL DEGREES OF FREEDOM =
SIZE OF STIFFNESS MATRIX = 103936 DOUBLE PREC. WORDS
TOTAL REQUIRED DISK SPACE = 14.25 MEGA-BYTES
447. PAGE NEW
812
33


********x*x*x*******************x**************x*****
448. *
449. PERFORM ANALYSIS
++ PROCESSING ELEMENT STIFFNESS MATRIX. 21:46:27
++ PROCESSING GLOBAL STIFFNESS MATRIX. 21:46:32
++ PROCESSING TRIANGULAR FACTORIZATION. 21:47:37
++ CALCULATING JOINT DISPLACEMENTS. 21:48:56
++ CALCULATING ELEMENT FORCES. 21:49:12
450. *
451. LOAD LIST 100,110,120,130,140
452. *
453. PAGE NEW
34


STAAD SPACE
455. ****SUPPORT REACTIONS*********
457. PRINT SUPPORT REACTIONS
35


STAAD SPACE
*****************************************************
SUPPORT REACTIONS -UNIT POUN INCH STRUCTURE TYPE = SPACE
JOINT LOAD FORCE-X FORCE-Y FORCE-Z MOM-X MOM-Y MOM
89 100 0.00 2304.96 0.00 0.00 0.00 0.
110 0.00 2582.94 0.00 0.00 0.00 0.
120 0.00 1153.89 0.00 0.00 0.00 0.
130 0.00 2610.57 0.00 0.00 0.00 0.
140 0.00 1337.31 0.00 0.00 0.00 0.
90 100 0.00 2925.88 0.00 0.00 0.00 0.
110 0.00 2879.56 0.00 0.00 0.00 0.
120 0.00 1606.02 0.00 0.00 0.00 0.
130 0.00 4122.77 0.00 0.00 0.00 0.
140 0.00 2151.24 0.00 0.00 0.00 0.
91 100 0.00 2995.91 0.00 0.00 0.00 0.
110 0.00 2292.70 0.00 0.00 0.00 0.
120 0.00 3191.41 0.00 0.00 0.00 0.
130 0.00 3951.84 0.00 0.00 0.00 0.
140 0.00 3766.12 0.00 0.00 0.00 0.
92 100 0.00 2911.63 0.00 0.00 0.00 0.
110 0.00 2320.86 0.00 0.00 0.00 0.
120 0.00 3159.06 0.00 0.00 0.00 0.
130 0.00 2804.46 0.00 0.00 0.00 0.
140 0.00 3354.97 0.00 0.00 0.00 0.
96 100 453.86 404.49 -159.17 0.00 0.00 0.
110 327.97 409.20 -8.09 0.00 0.00 0.
120 306.91 492.14 429.87 0.00 0.00 0.
130 185.06 340.57 -70.88 0.00 0.00 0.
140 -20.40 421.70 538.07 0.00 0.00 0.
100 100 940.37 576.71 159.17 0.00 0.00 0.
110 698.42 579.78 247.28 0.00 0.00 0.
120 579.45 697.19 702.54 0.00 0.00 0.
130 338.94 485.09 70.88 0.00 0.00 0.
140 -140.40 588.69 594.31 0.00 0.00 0.
104 100 -449.56 438.14 -161.10 0.00 0.00 0.
110 -327.14 427.67 -8.77 0.00 0.00 0.
120 -304.29 516.89 428.95 0.00 0.00 0.
130 -170.43 355.49 -75.54 0.00 0.00 0.
140 26.40 443.44 536.66 0.00 0.00 0.
108 100 -944.66 623.76 161.10 0.00 0.00 0.
110 -699.25 605.70 247.96 0.00 0.00 0.
120 -582.06 731.81 703.45 0.00 0.00 0.
130 -353.58 501.90 75.51 0.00 0.00 0.
140 134.39 617.51 595.73 0.00 0.00 0.
Z
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
00
36


STAAD SPACE
************** END OF LATEST ANALYSIS RESULT **************
458. PAGE NEW
37


STAAD SPACE
459, **********x*******************
460. ****JOINT DISPLACEMENT********
462. PRINT JOINT DISPLACEMENTS
38


STAAD SPACE
*****************************************************
JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
1 100 -0.00539 0.02220 -0.05511 0.00074 -0.00013 -0.00129
110 0.00179 -0.00912 0.00684 -0.00015 0.00000 -0.C0334
120 -0.00241 0.06662 -0.13154 0.00133 -0.00007 -0.00179
130 0.01527 0.11801 -0.01039 0.00057 -0.00033 -0.00204
140 0.03342 0.15206 -0.08962 0.00130 -0.00015 -0.00186
2 100 -0.00531 -0.01161 -0.05306 0.00192 -0.00012 0.00128
110 0.00191 -0.17636 0.00520 -0.00072 0.00003 0.00450
120 -0.00233 -0.00481 -0.13100 0.00182 -0.00006 0.00216
130 -0.01520 0.03445 0.00282 0.00092 -0.00033 0.00193
140 0.00295 0.07722 -0.08521 0.00172 -0.00014 0.00209
3 100 -0.00526 0.02220 -0.05029 0.00109 -0.00016 0.00003
110 0.00197 -0.01238 0.00400 0.00007 0.00004 0.00301
120 -0.00228 0.06639 -0.12978 0.00159 -0.00009 0.00096
130 -0.02946 0.10029 0.00997 0.00059 -0.00035 0.00070
140 -0.01130 0.14664 -0.08213 0.00145 -0.00017 0.00088
4 100 -0.00522 -0.01835 -0.04450 0.00188 -0.00026 -0.00114
110 0.00199 -0.02187 0.00362 0.00158 -0.00002 -0.00103
120 -0.00225 0.03987 -0.12645 0.00252 -0.00016 -0.00099
130 -0.04566 0.06704 0.02036 0.00145 -0.00044 -0.00125
140 -0.02751 0.11816 -0.07651 0.00236 -0.00025 -0.00108
5 100 -0.00515 0.02557 -0.03120 0.00050 -0.00024 0.00163
110 0.00203 0.00387 0.00621 0.00012 -0.00005 0.00139
120 -0.00220 0.07360 -0.11771 0.00128 -0.00016 0.00139
130 -0.07421 0.08791 0.04202 0.00010 -0.00043 0.00113
140 -0.05606 0.14737 -0.06350 0.00112 -0.00025 0.00130
6 100 -0.01166 0.01322 -0.05510 0.00067 -0.00012 -0.00172
110 0.00094 -0.00417 0.00684 -0.00013 0.00001 -0.00264
120 -0.00631 0.03306 -0.13154 0.00128 -0.00007 -0.00182
130 0.00318 0.10653 -0.03119 0.00051 -0.00032 -0.00207
140 0.02697 0.11884 -0.11042 0.00125 -0.00015 -0.00189
7 100 -0.01163 -0.09321 -0.05306 0.00127 -0.00015 -0.00019
110 0.00102 -0.13431 0.00521 -0.00032 0.00000 0.00075
120 -0.00627 -0.06882 -0.13100 0.00157 -0.00009 0.00013
130 -0.02733 -0.00119 -0.01797 0.00067 -0.00035 -0.00009
140 -0.00354 0.01652 -0.10601 0.00148 -0.00017 0.00006
8 100 -0.01163 -0.09986 -0.04946 0.00126 -0.00018 -0.00023
110 0.00104 -0.11972 0.00431 0.00017 0.00006 0.00065
120 -0.00626 -0.06788 -0.12917 0.00173 -0.00009 0.00008
130 -0.04163 -0.00338 -0.01012 0.00076 -0.00037 -0.00002
39


STAAD SPACE
*****************************************************
JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS
140 -0.01784 0.01670
9 100 -0.01162 -0.09915
110 0.00106 -0.10499
120 -0.00625 -0.06272
130 -0.05787 -0.00163
140 -0.03408 0.02079
10 100 -0.01160 0.02500
110 0.00108 0.01125
120 -0.00624 0.04562
130 -0.08646 0.10125
140 -0.06267 0.12600
11 100 0.02470 -0.01113
110 0.01421 -0.00750
120 0.01355 -0.02803
130 0.09715 0.07483
140 0.06875 0.05867
12 100 0.02472 -0.12302
110 0.01427 -0.07524
120 0.01375 0.01048
130 0.06856 -0.01488
140 0.04034 0.10074
13 100 0.02473 -0.11751
110 0.01431 -0.06908
120 0.01390 0.02355
130 0.05231 -0.00730
140 0.02424 0.11476
14 100 0.02474 -0.10538
110 0.01434 -0.06337
120 0.01404 0.01353
130 0.03801 0.00548
140 0.01008 0.10533
15 100 0.02477 0.01480
110 0.01441 0.01308
120 0.01425 -0.00569
130 0.00748 0.11158
140 -0.02026 0.08594
16 100 0.01692 -0.02922
110 0.01018 -0.01700
120 0.01225 -0.08494
Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
-0.10227 0.00162 -0.00018 0.00006
-0.04449 0.00126 -0.00022 0.00026
0.00361 0.00074 -0.00003 0.00039
-0.12645 0.00190 -0.00014 0.00026
-0.00044 0.00086 -0.00041 0.00005
-0.09731 0.00177 -0.00023 0.00018
-0.03119 0.00044 -0.00026 0.00230
0.00621 0.00003 -0.00006 0.00213
-0.11770 0.00121 -0.00017 0.00202
0.02123 0.00005 -0.00045 0.00182
-0.08430 0.00105 -0.00026 0.00196
-0.02742 0.00015 -0.00031 -0.00202
-0.19686 0.00142 -0.00010 -0.00145
-1.05392 0.00832 0.00029 -0.00029
-0.06470 0.00034 -0.00054 -0.00153
-1.07593 0.00833 0.00019 -0.00021
-0.01225 -0.00069 -0.00026 0.00001
-0.19741 0.00097 -0.00006 0.00023
-1.09421 0.00880 0.00033 0.00117
-0.03877 -0.00048 -0.00049 0.00021
-1.11164 0.00880 0.00024 0.00125
-0.00633 -0.00071 -0.00022 0.00048
-0.19532 0.00099 -0.00011 0.00031
-1.09723 0.00887 -0.00009 0.00000
-0.02669 -0.00057 -0.00047 0.00048
-1.11224 0.00884 -0.00019 0.00001
-0.00189 -0.00072 -0.00019 0.00045
-0.19214 0.00100 -0.00018 0.00007
-1.09107 0.00893 -0.00047 -0.00099
-0.01682 -0.00064 -0.00043 0.00057
-1.10400 0.00888 -0.00056 -0.00094
0.00212 -0.00011 -0.00017 0.00201
-0.18150 0.00127 -0.00015 0.00149
-1.04213 0.00814 -0.00041 0.00078
-0.00064 -0.00026 -0.00040 0.00193
-1.05073 0.00803 -0.00050 0.00084
-0.02741 0.00008 -0.00028 -0.00133
-0.19688 0.00126 -0.00002 -0.00118
-1.05402 0.00779 0.00057 -0.00118
40


STAAD SPACE
*****************************************************
JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
130 0.08227 0.04850 -0.08549 0.00029 -0.00051 -0.00089
140 0.06461 -0.00014 -1.09683 0.00781 0.00048 -0.00108
17 100 0.01699 -0.06062 -0.01225 -0.00130 -0.00030 0.00141
110 0.01020 -0.05231 -0.19744 0.00005 -0.00012 0.00136
120 0.01211 -0.14380 -1.09434 0.00638 0.00017 0.00210
130 0.05373 0.03405 -0.05957 -0.00098 -0.00054 0.00146
140 0.03588 -0.05425 -1.13257 0.00639 0.00007 0.00218
18 100 0.01703 -0.01318 -0.00549 -0.00052 -0.00020 0.00025
110 0.01020 -0.00627 -0.19444 0.00131 -0.00010 0.00015
120 0.01197 -0.07324 -1.09571 0.00980 -0.00009 0.00007
130 0.03752 0.08072 -0.04668 -0.00039 -0.00044 0.00045
140 0.01950 0.01821 -1.13147 0.00977 -0.00018 0.00015
19 100 0.01708 -0.04103 -0.00189 -0.00137 -0.00016 -0.00101
110 0.01021 -0.03785 -0.19217 0.00001 -0.00011 -0.00116
120 0.01185 -0.13023 -1.09122 0.00627 -0.00025 -0.00210
130 0.02326 0.06161 -0.03762 -0.00120 -0.00041 -0.00066
140 0.00507 -0.03705 -1.12495 0.00622 -0.00034 -0.00203
20 100 0.01716 0.00623 0.00212 -0.00020 -0.00017 0.00158
110 0.01023 0.00789 -0.18152 0.00110 -0.00022 0.00137
120 0.01170 -0.05609 -1.04223 0.00762 -0.00071 0.00162
130 -0.00722 0.11226 -0.02144 -0.00035 -0.00040 0.00157
140 -0.02563 0.04016 -1.07163 0.00750 -0.00080 0.00168
21 100 -0.00606 0.02227 -0.02993 0.00059 0.00002 -0.00031
110 0.00053 -0.00894 0.00351 -0.00006 0.00010 -0.00006
120 -0.00361 0.06672 -0.08387 0.00127 0.00008 -0.00019
130 0.02317 0.09471 0.00935 0.00048 -0.00004 -0.00044
140 0.03493 0.12876 -0.04319 0.00122 0.00007 -0.00027
22 100 -0.00612 0.02216 -0.02049 0.00067 -0.00011 0.00007
110 -0.00143 -0.01242 0.00346 -0.00006 -0.00001 -0.00059
120 -0.00409 0.06635 -0.07924 0.00130 -0.00007 -0.00014
130 -0.02161 0.07685 0.02457 0.00031 -0.00026 -0.00040
140 -0.01007 0.12320 -0.03632 0.00117 -0.00013 -0.00022
23 100 -0.00618 0.02564 -0.01483 0.00038 -0.00027 0.00000
110 -0.00329 0.00393 0.00694 -0.00006 -0.00017 0.00001
120 -0.00454 0.07365 -0.07370 0.00115 -0.00024 0.00001
130 -0.06636 0.06456 0.04511 0.00003 -0.00051 -0.00031
140 -0.05504 0.12402 -0.02482 0.00100 -0.00037 -0.00010
24 100 -0.00313 0.01336 -0.02994 0.00059 0.00001 -0.00068
110 0.00645 -0.00405 0.00350 -0.00008 0.00017 -0.00051
41


STAAD SPACE
A****************************************************
JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
120 0.00079 0.03317 -0.08387 0.00128 0.00008 -0.00057
130 0.02277 0.08323 -0.01145 0.00051 -0.00009 -0.00088
140 0.03866 0.09555 -0.06399 0.00125 0.00004 -0.00069
25 100 -0.00314 -0.09321 -0.02203 0.00058 -0.00021 -0.00064
110 0.00641 -0.13424 0.00128 -0.00001 -0.00012 -0.00069
120 0.00077 -0.06879 -0.08025 0.00128 -0.00016 -0.00058
130 -0.00781 -0.02457 0.00026 0.00038 -0.00034 -0.00082
140 0.00808 -0.00685 -0.05824 0.00121 -0.00021 -0.00064
26 100 -0.00313 -0.09917 -0.01356 0.00053 -0.00015 -0.00032
110 0.00641 -0.10504 0.01320 -0.00006 -0.00025 0.00009
120 0.00078 -0.06275 -0.07139 0.00124 -0.00018 -0.00016
130 -0.03835 -0.02506 0.01743 0.00022 -0.00035 -0.00049
140 -0.02246 -0.00263 -0.04669 0.00113 -0.00024 -0.00027
27 100 -0.01958 0.02515 -0.01484 0.00034 -0.00044 -0.00057
110 -0.01172 0.01137 0.00693 -0.00006 -0.00027 -0.00040
120 -0.01623 0.04574 -0.07371 0.00114 -0.00038 -0.00042
130 -0.08642 0.07799 0.02430 -0.00001 -0.00063 -0.00076
140 -0.07071 0.10272 -0.04562 0.00100 -0.00049 -0.00049
28 100 0.02352 -0.01098 -0.02256 0.00025 -0.00051 0.00079
110 0.01398 -0.00747 -0.12935 0.00205 -0.00032 0.00051
120 0.00757 -0.02834 -0.67489 0.01103 -0.00004 0.00017
130 0.08716 0.05156 -0.05376 0.00041 -0.00071 0.00096
140 0.06066 0.03496 -0.69679 0.01104 -0.00017 0.00022
29 100 0.00710 -0.12304 -0.02280 0.00004 -0.00017 0.00055
110 0.00369 -0.07527 -0.13996 0.00209 -0.00006 0.00027
120 0.01158 0.01041 -0.71698 0.01177 0.00010 -0.00023
130 0.04171 -0.03830 -0.04404 0.00012 -0.00033 0.00078
140 0.03389 0.07727 -0.73495 0.01175 0.00004 -0.00013
30 100 0.00711 -0.10538 -0.01340 -0.00003 -0.00024 0.00091
110 0.00370 -0.06339 -0.13303 0.00207 -0.00027 0.00062
120 0.01160 0.01343 -0.70661 0.01177 -0.00065 0.00021
130 0.01116 -0.01792 -0.02739 -0.00005 -0.00038 0.00098
140 0.00336 0.08183 -0.72172 0.01171 -0.00071 0.00027
31 100 0.00709 0.01494 -0.00333 -0.00005 -0.00006 0.00089
110 0.00369 0.01310 -0.11977 0.00190 -0.00012 0.00054
120 0.01161 -0.00600 -0.66852 0.01097 -0.00053 -0.00007
130 -0.01940 0.08829 -0.01111 -0.00022 -0.00020 0.00106
140 -0.02718 0.06223 -0.68136 0.01084 -0.00057 0.00004
32 100 0.00783 -0.02915 -0.02257 0.00022 -0.00033 0.00024


STAAD SPACE
kirk**************************************************
JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
110 0.00383 -0.01685 -0.12938 0.00209 -0.00020 0.00012
120 0.00493 -0.08445 -0.67503 0.01127 -0.00003 0.00002
130 0.06486 0.02515 -0.07457 0.00036 -0.00055 0.00050
140 0.05383 -0.02306 -0.71772 0.01127 -0.00015 0.00012
33 100 0.00777 -0.01323 -0.01450 -0.00009 -0.00013 0.00022
110 0.00370 -0.00631 -0.13287 0.00192 -0.00006 0.00017
120 0.00446 -0.07328 -0.70623 0.01131 -0.00004 0.00025
130 0.02089 0.05728 -0.05233 -0.00003 -0.00031 0.00043
140 0.00900 -0.00523 -0.74294 0.01128 -0.00011 0.00034
34 100 0.00770 0.00630 -0.00333 -0.00003 -0.00001 0.00055
110 0.00356 0.00803 -0.11980 0.00196 0.00000 0.00040
120 0.00398 -0.05561 -0.66864 0.01118 -0.00011 0.00031
130 -0.02308 0.08893 -0.03191 -0.00018 -0.00013 0.00068
140 -0.03584 0.01725 -0.70228 0.01106 -0.00013 0.00038
35 100 -0.00816 0.02308 -0.00494 0.00036 0.00013 0.00009
110 -0.00631 -0.00749 0.00071 -0.00011 0.00010 0.00003
120 -0.00883 0.06776 -0.02351 0.00118 0.00017 0.00011
130 0.02931 0.06493 0.03463 0.00045 0.00018 -0.00015
140 0.03166 0.09882 0.01724 0.00120 0.00024 0.00007
36 100 -0.00046 0.02648 -0.00099 0.00010 -0.00010 0.00028
110 -0.00119 0.00523 0.00216 -0.00019 -0.00005 0.00032
120 0.00093 0.07465 -0.02039 0.00101 -0.00012 0.00024
130 -0.04299 0.03468 0.04455 -0.00028 -0.00032 -0.00001
140 -0.04202 0.09402 0.02249 0.00084 -0.00024 0.00012
37 100 -0.00377 0.01368 -0.00490 0.00041 0.00005 -0.00009
110 -0.00263 -0.00376 0.00075 -0.00005 0.00008 -0.00037
120 -0.00319 0.03345 -0.02350 0.00118 0.00010 0.00005
130 0.03560 0.05229 0.01389 0.00051 0.00010 -0.00006
140 0.03943 0.06463 -0.00355 0.00120 0.00014 0.00023
38 100 -0.00327 0.02541 -0.00094 0.00018 -0.00004 0.00062
110 -0.00235 0.01158 0.00221 -0.00014 -0.00001 0.00070
120 -0.00254 0.04597 -0.02037 0.00102 -0.00006 0.00038
130 -0.05320 0.04703 0.02385 -0.00009 -0.00022 -0.00006
140 -0.04926 0.07175 0.00173 0.00089 -0.00014 0.00001
39 100 -0.00300 -0.01072 -0.00822 0.00041 -0.00007 -0.00031
110 -0.00289 -0.00753 -0.01830 0.00151 0.00003 -0.00014
120 -0.00111 -0.02946 -0.09355 0.00796 0.00033 0.00049
130 0.04521 0.02061 -0.03291 0.00056 -0.00025 0.00034
140 0.04494 0.00264 -0.11569 0.00796 0.00024 0.00090
43


STAAD SPACE
*****************************************************
JOINT DISPLACEMENT (INCH RADIANS;
STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
40 100 -0.00268 0.01526 -0.00315 0.00012 0.00000 0.00063
110 -0.00265 0.01309 -0.01556 0.00137 -0.00009 0.00043
120 -0.00103 -0.00712 -0.09003 0.00781 -0.00044 0.00023
130 -0.04369 0.05734 -0.02099 -0.00016 0.00005 0.00041
140 -0.04424 0.02989 -0.10972 0.00764 -0.00040 0.00000
41 100 -0.00683 -0.02831 -0.00816 0.00049 -0.00013 0.00009
110 -0.00541 -0.01583 -0.01829 0.00151 -0.00011 0.00014
120 -0.00135 -0.08236 -0.09363 0.00783 -0.00012 0.00051
130 0.03370 -0.00476 -0.05363 0.00069 -0.00035 0.00033
140 0.04023 -0.05187 -0.13655 0.00787 -0.00025 0.00064
42 100 -0.00087 0.00711 -0.00311 0.00016 0.00008 0.00034
110 -0.00234 0.00902 -0.01556 0.00135 0.00005 0.00022
120 -0.00547 -0.05350 -0.09013 0.00767 -0.00001 0.00011
130 -0.03931 0.05905 -0.04174 -0.00012 0.00014 0.00047
140 -0.04665 -0.01152 -0.13060 0.00753 0.00005 0.00014
43 100 -0.00763 0.02336 0.00073 0.00042 -0.00003 -0.00031
110 -0.00729 -0.00699 -0.00074 0.00001 -0.00001 -0.00001
120 -0.00725 0.06811 -0.00478 0.00117 0.00002 -0.00045
130 0.03726 0.05501 0.04234 0.00060 0.00002 -0.00103
140 0.03701 0.08885 0.03636 0.00121 0.00007 -0.00092
44 100 -0.00764 0.01772 0.00278 0.00082 -0.00007 -0.00001
110 -0.00730 -0.00680 0.00038 0.00028 -0.00005 0.00006
120 -0.00725 0.06175 -0.00528 0.00168 -0.00001 0.00004
130 0.01613 0.03579 0.04186 0.00149 -0.00001 -0.00017
140 0.01588 0.07510 0.03325 0.00199 0.00005 0.00000
45 100 -0.00765 0.01916 0.00403 0.00087 -0.00006 0.00014
110 -0.00730 -0.00487 0.00119 0.00032 -0.00004 0.00015
120 -0.00726 0.06439 -0.00475 0.00174 -0.00005 0.00022
130 0.00540 0.03585 0.04240 0.00155 -0.00004 0.00006
140 0.00516 0.07804 0.03300 ' 0.00208 -0.00002 0.00025
46 100 -0.00766 0.02129 0.00455 0.00080 -0.00003 0.00018
110 -0.00731 -0.00285 0.00160 0.00028 -0.00003 0.00017
120 -0.00726 0.06736 -0.00412 0.00168 -0.00006 0.00024
130 -0.00176 0.03663 0.04277 0.00144 -0.00003 -0.00004
140 -0.00199 0.08132 0.03342 0.00197 -0.00005 0.00023
47 100 -0.00766 0.02226 0.00476 0.00075 -0.00001 -0.00001
110 -0.00731 -0.00170 0.00183 0.00025 -0.00002 0.00004
120 -0.00727 0.06882 -0.00355 0.00162 -0.00006 0.00002
130 -0.00761 0.03458 0.04294 0.00135 -0.00001 -0.00051
44


STAAD SPACE
*****************************************************
JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
140 -0.00784 0.08215 0.03395 0.00189 -0.00006 -0.00013
48 100 -0.00767 0.02099 0.00474 0.00073 0.00002 -0.00023
110 -0.00732 -0.00209 0.00193 0.00024 0.00000 -0.00010
120 -0.00727 0.06770 -0.00305 0.00160 -0.00005 -0.00023
130 -0.01347 0.02735 0.04289 0.00135 0.00002 -0.00100
140 -0.01370 0.07882 0.03448 0.00187 -0.00006 -0.00053
49 100 -0.00769 0.01471 0.00330 0.00066 0.00008 0.00001
110 -0.00733 -0.00454 0.00124 0.00021 0.00005 0.00009
120 -0.00729 0.06089 -0.00273 0.00155 0.00004 0.00000
130 -0.03169 0.00171 0.04172 0.00137 0.00005 -0.00024
140 -0.03191 0.06354 0.03549 0.00183 -0.00001 -0.00012
50 100 -0.00772 0.02676 0.00063 0.00018 -0.00001 0.00073
110 -0.00735 0.00567 -0.00064 -0.00008 0.00000 0.00051
120 -0.00731 0.07499 -0.00442 0.00101 -0.00001 0.00090
130 -0.05252 0.02472 0.04078 -0.00001 -0.00007 0.00141
140 -0.05273 0.08403 0.03598 0.00090 -0.00008 0.00138
51 100 -0.00938 0.02554 0.00042 -0.00009 -0.00002 0.00132
110 -0.00818 0.01169 -0.00093 -0.00033 -0.00001 0.00074
120 -0.00842 0.04608 -0.00461 0.00093 0.00000 0.00186
130 -0.05441 0.03676 0.01963 -0.00064 0.00000 0.00222
140 -0.05384 0.06147 0.01494 0.00069 0.00004 0.00281
52 100 -0.00938 0.02620 0.00037 0.00017 0.00001 0.00160
110 -0.00812 0.01448 -0.00101 -0.00004 0.00001 0.00085
120 -0.00819 0.03735 -0.00467 0.00103 0.00003 0.00231
130 -0.05410 0.04231 0.01369 -0.00025 0.00003 0.00265
140 -0.05330 0.05475 0.00903 0.00086 0.00004 0.00348
53 100 -0.01019 0.02222 0.00026 0.00031 -0.00004 0.00230
110 -0.00872 0.01279 -0.00114 0.00017 -0.00003 0.00157
120 -0.00886 0.02521 -0.00477 0.00078 -0.00003 0.00253
130 -0.05415 0.04193 0.00560 0.00012 0.00000 0.00374
140 -0.05315 0.04431 0.00098 0.00067 0.00001 0.00400
54 100 -0.01167 0.01965 0.00013 0.00019 -0.00014 0.00206
110 -0.00984 0.01189 -0.00129 0.00000 -0.00011 0.00150
120 -0.01001 0.01822 -0.00490 0.00050 -0.00010 0.00201
130 -0.05447 0.04152 -0.00168 -0.00007 -0.00004 0.00372
140 -0.05299 0.03911 -0.00626 0.00029 0.00001 0.00362
55 100 -0.01226 0.01781 0.00000 0.00017 0.00013 0.00203
110 -0.01030 0.01238 -0.00144 -0.00004 0.00010 0.00157
120 -0.01039 0.01414 -0.00520 0.00029 0.00012 0.00168
45


STAAD SPACE
*****************************************************
JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
130 -0.05463 0.04315 -0.00892 -0.00018 0.00006 0.00404
140 -0.05289 0.03772 -0.01366 0.00001 0.00003 0.00359
56 100 -0.00977 0.01802 -0.00006 0.00004 0.00015 0.00116
110 -0.00848 0.01440 -0.00155 -0.00008 0.00011 0.00091
120 -0.00877 0.00680 -0.00558 0.00105 0.00011 0.00051
130 -0.05372 0.04693 -0.01697 -0.00025 0.00005 0.00309
140 -0.05322 0.03242 -0.02201 0.00092 -0.00001 0.00223
57 100 -0.00906 0.01541 -0.00010 0.00032 0.00004 0.00106
110 -0.00796 0.01308 -0.00164 0.00021 0.00003 0.00084
120 -0.00835 -0.00765 -0.00588 0.00181 0.00001 0.00057
130 -0.05367 0.04706 -0.02287 0.00001 0.00000 0.00265
140 -0.05363 0.01896 -0.02817 0.00169 -0.00005 0.00195
58 100 -0.00870 0.00738 -0.00026 0.00015 0.00007 0.00075
110 -0.00787 0.00939 -0.00192 0.00017 0.00004 0.00059
120 -0.00892 -0.05262 -0.00674 0.00197 -0.00003 0.00055
130 -0.05357 0.04909 -0.04390 -0.00023 0.00007 0.00148
140 -0.05458 -0.02094 -0.04987 0.00175 -0.00003 0.00113
59 100 -0.00871 -0.00983 0.00326 -0.00021 0.00009 0.00029
110 -0.00788 -0.00420 0.00028 -0.00006 0.00006 0.00022
120 -0.00891 -0.06701 -0.00691 0.00224 0.00004 0.00028
130 -0.03244 0.01903 -0.04126 -0.00097 0.00004 0.00042
140 -0.03344 -0.04439 -0.05154 0.00172 -0.00002 0.00032
60 100 -0.00872 -0.01255 0.00426 -0.00024 0.00003 0.00008
110 -0.00788 -0.00600 0.00104 -0.00003 0.00002 0.00003
120 -0.00891 -0.06995 -0.00633 0.00255 0.00000 0.00010
130 -0.02171 0.01547 -0.04092 -0.00095 0.00000 0.00014
140 -0.02270 -0.04669 -0.05190 0.00202 -0.00004 0.00003
61 100 -0.00872 -0.01309 0.00440 -0.00011 -0.00002 0.00014
110 -0.00788 -0.00571 0.00093 0.00021 -0.00002 0.00008
120 -0.00891 -0.07082 -0.00714 0.00337 -0.00003 0.00011
130 -0.00870 0.01045 -0.04098 -0.00062 -0.00001 0.00069
140 -0.00967 -0.04714 -0.05307 0.00294 -0.00002 0.00025
62 100 -0.00873 -0.01605 0.00404 -0.00009 -0.00004 0.00029
110 -0.00788 -0.00769 0.00060 0.00013 -0.00005 0.00020
120 -0.00890 -0.07297 -0.00753 0.00295 -0.00008 0.00020
130 -0.00089 -0.00164 -0.04100 -0.00052 0.00000 0.00112
140 -0.00186 -0.05240 -0.05312 0.00255 -0.00003 0.00051
63 100 -0.00876 -0.02802 -0.00030 0.00041 -0.00002 0.00006
110 -0.00790 -0.01545 -0.00222 0.00029 0.00001 0.00005
46


STAAD SPACE
************T***************************************
JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
120 -0.00889 -0.08149 -0.00722 0.00216 0.00010 0.00015
130 0.03616 -0.01473 -0.04255 0.00056 -0.00004 -0.00085
140 0.03525 -0.06131 -0.04963 0.00215 0.00007 -0.00038
64 100 -0.00916 -0.01059 -0.00006 0.00070 -0.00004 0.00033
110 -0.00823 -0.00755 -0.00186 0.00040 -0.00004 0.00033
120 -0.00934 -0.02999 -0.00629 0.00208 -0.00009 0.00066
130 0.03670 0.01034 -0.02133 0.00104 0.00000 -0.00103
140 0.03592 -0.00828 -0.02781 0.00220 -0.00004 -0.00055
65 100 -0.00839 -0.00457 0.00001 0.00037 -0.00016 0.00039
110 -0.00751 -0.00454 -0.00175 0.00008 -0.00013 0.00039
120 -0.00817 -0.01306 -0.00598 0.00128 -0.00018 0.00085
130 0.03664 0.01951 -0.01537 0.00060 -0.00003 -0.00124
140 0.03617 0.00987 -0.02163 0.00135 -0.00003 -0.00069
66 100 -0.00574 -0.00207 0.00010 0.00029 -0.00015 -0.00058
110 -0.00546 -0.00546 -0.00161 -0.00001 -0.00011 -0.00028
120 -0.00596 -0.00381 -0.00557 0.00037 -0.00016 -0.00037
130 0.03735 0.02326 -0.00725 0.00020 -0.00005 -0.00266
140 0.03614 0.01888 -0.01323 0.00019 -0.00005 -0.00224
67 100 -0.00619 0.00119 0.00026 0.00035 0.00013 -0.00078
110 -0.00577 -0.00561 -0.00144 0.00006 0.00010 -0.00029
120 -0.00596 0.00119 -0.00524 0.00061 0.00008 -0.00083
130 0.03708 0.02585 0.00006 0.00035 0.00005 -0.00268
140 0.03642 0.02222 -0.00579 0.00049 -0.00002 -0.00246
68 100 -0.00763 0.00579 0.00039 0.00049 0.00004 -0.00110
110 -0.00682 -0.00377 -0.00128 0.00024 0.00003 -0.00037
120 -0.00684 0.00964 -0.00510 0.00091 0.00001 -0.00140
130 0.03652 0.03115 0.00731 0.00060 0.00003 -0.00304
140 0.03664 0.02993 0.00144 0.00090 -0.00002 -0.00297
69 100 -0.00842 0.01213 0.00049 0.00037 -0.00002 -0.00063
110 -0.00739 -0.00132 -0.00113 -0.00001 -0.00002 0.00023
120 -0.00735 0.02337 -0.00500 0.00115 -0.00003 -0.00136
130 0.03614 0.03916 0.01537 0.00052 -0.00001 -0.00242
140 0.03671 0.04388 0.00947 0.00119 -0.00003 -0.00274
70 100 -0.00821 0.01383 0.00054 0.00019 -0.00002 -0.00054
110 -0.00730 -0.00363 -0.00105 -0.00025 -0.00001 0.00015
120 -0.00721 0.03358 -0.00496 0.00111 -0.00001 -0.00108
130 0.03646 0.04202 0.02128 0.00031 -0.00004 -0.00204
140 0.03698 0.05435 0.01537 0.00113 -0.00002 -0.00219
71 100 -0.00852 -0.02391 0.00325 0.00081 -0.00002 -0.00284
47


STAAD SPACE
xXXXXXXXXxXxXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXXX
JOINT DISPLACEMENT (INCH RADIANS
JOINT LOAD X-TRANS Y-TRANS
110 -0.00746 -0.01494
120 -0.00743 -0.02618
130 0.02047 -0.04593
140 0.02107 -0.04212
72 100 -0.00866 -0.08856
110 -0.00757 -0.06491
120 -0.00754 -0.08691
130 0.00869 -0.14823
140 0.00935 -0.12803
73 100 -0.00872 -0.11450
110 -0.00761 -0.08607
120 -0.00759 -0.11040
130 0.00412 -0.18462
140 0.00479 -0.15856
74 100 -0.00890 -0.16238
110 -0.00775 -0.12631
120 -0.00775 -0.15374
130 -0.01012 -0.24380
140 -0.00940 -0.21094
75 100 -0.00920 -0.06873
110 -0.00798 -0.05213
120 -0.00801 -0.06882
130 -0.03319 -0.10283
140 -0.03240 -0.09607
76 100 -0.00922 -0.06036
110 -0.00800 -0.04555
120 -0.00803 -0.06093
130 -0.03450 -0.09045
140 -0.03370 -0.08528
77 100 -0.00927 -0.03545
110 -0.00803 -0.02620
120 -0.00807 -0.03699
130 -0.03842 -0.05352
140 -0.03762 -0.05221
78 100 -0.00854 -0.01471
110 -0.00761 -0.01108
120 -0.00820 -0.00861
130 0.02095 -0.03666
140 0.02063 -0.02749
STRUCTURE TYPE = SPACE
TRANS X-RCTAN Y-ROTAN Z-ROTAN
.00128 0.00073 -0.00001 -0.00199
.00175 0.00077 0.00001 -0.00285
.01577 0.00114 0.00001 -0.00508
.01015 0.00111 0.00004 -0.00444
.00398 0.00209 -0.00003 -0.00381
.00136 0.00177 0.00001 -0.00307
.00373 0.00192 0.00014 -0.00346
.01580 0.00299 0.00000 -0.00552
.00744 0.00255 0.00016 -0.00460
.00410 0.00259 -0.00002 -0.00348
.00123 0.00217 0.00002 -0.00286
.00473 0.00239 0.00013 -0.00315
.01582 0.00352 -0.00001 -0.00475
.00636 0.00307 0.00013 -0.00403
.00416 0.00399 0.00001 -0.00022
.00080 0.00341 0.00000 -0.00024
.00705 0.00353 0.00000 -0.00023
.01587 0.00486 0.00001 0.00008
.00417 0.00424 0.00000 -0.00012
.00336 0.00204 0.00003 0.00414
.00130 0.00175 0.00000 0.00325
.00265 0.00187 -0.00010 0.00389
.01511 0.00193 0.00002 0.00610
.00889 0.00215 -0.00011 0.00531
.00331 0.00193 0.00003 0.00416
.00130 0.00167 0.00000 0.00326
.00246 0.00177 -0.00008 0.00395
.01507 0.00183 0.00002 0.00615
.00911 0.00203 -0.00010 0.00541
.00306 0.00116 0.00003 0.00391
.00120 0.00102 0.00001 0.00299
.00215 0.00108 -0.00002 0.00384
.01490 0.00113 0.00002 0.00586
.00957 0.00131 -0.00003 0.00539
.00339 -0.00078 -0.00017 -0.00208
.00140 -0.00066 -0.00013 -0.00161
.00156 -0.00067 -0.00011 -0.00152
.01443 -0.00118 -0.00005 -0.00435
.02001 -0.00102 0.00003 -0.00338
;)
z-1
0
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0
0
0
0
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0
0
0
0
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0
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0
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0
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0
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0
0
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0
0
0
0
-0
-0
-0
48


STAAD SPACE
*****************************************************
JOINT DISPLACEMENT (INCH RADIANS
JOINT LOAD X-TRANS Y-TRANS
79 100 -0.00876 -0.07107
110 -0.00776 -0.05678
120 -0.00829 -0.05367
130 0.00915 -0.13059
140 0.00898 -0.10120
80 100 -0.00893 -0.12041
110 -0.00788 -0.09789
120 -0.00837 -0.09506
130 -0.00068 -0.19795
140 -0.00073 -0.15614
81 100 -0.00910 -0.14277
110 -0.00800 -0.11685
120 -0.00844 -0.11431
130 -0.00969 -0.22338
140 -0.00963 -0.17846
82 100 -0.00931 -0.11667
110 -0.00815 -0.09543
120 -0.00854 -0.09300
130 -0.02166 -0.18129
140 -0.02145 -0.14683
83 100 -0.00954 -0.05087
110 -0.00831 -0.04126
120 -0.00866 -0.03891
130 -0.03410 -0.08350
140 -0.03376 -0.06822
84 100 -0.00961 -0.02902
110 -0.00837 -0.02343
120 -0.00870 -0.02135
130 -0.03803 -0.04980
140 -0.03765 -0.04033
85 100 -0.00829 -0.04617
110 -0.00738 -0.03837
120 -0.00740 -0.03627
130 0.01524 -0.08453
140 0.01566 -0.05779
86 100 -0.00831 -0.08776
110 -0.00740 -0.06708
120 -0.00748 -0.08021
130 0.00450 -0.14562
STRUCTURE TYPE = SPACE
TRANS X-ROTAN Y-ROTAN Z-ROTAN
.00417 -0.00210 0.00001 -0.00357
.00147 -0.00178 0.00005 -0.00295
.00373 -0.00179 0.00023 -0.00296
.01433 -0.00319 0.00001 -0.00527
.02289 -0.00248 0.00022 -0.00420
.00406 -0.00315 0.00000 -0.00264
.00072 -0.00268 0.00003 -0.00221
.00706 -0.00265 0.00012 -0.00224
.01436 -0.00439 0.00000 -0.00333
.02604 -0.00350 0.00011 -0.00279
.00416 -0.00408 -0.00001 -0.00030
.00074 -0.00348 -0.00001 -0.00027
.00732 -0.00346 -0.00003 -0.00028
.01433 -0.00534 0.00000 -0.00002
.02631 -0.00434 -0.00003 -0.00016
.00426 -0.00305 0.00001 0.00274
.00111 -0.00260 -0.00003 0.00226
.00599 -0.00253 -0.00014 0.00226
.01431 -0.00392 0.00001 0.00409
.02496 -0.00326 -0.00014 0.00321
.00368 -0.00196 0.00007 0.00372
.00155 -0.00166 0.00002 0.00304
.00230 -0.00166 -0.00011 0.00302
.01498 -0.00230 0.00005 0.00564
.02119 -0.00208 -0.00014 0.00464
.00311 -0.00114 0.00016 0.00332
.00125 -0.00096 0.00011 0.00269
.00205 -0.00097 0.00007 0.00263
.01533 -0.00140 0.00008 0.00535
.02062 -0.00130 -0.00004 0.00445
.00275 0.00139 -0.00008 -0.00166
.00037 0.00067 -0.00005 -0.00105
.00531 0.00228 -0.00002 -0.00182
.02102 0.00212 -0.00004 -0.00291
.01241 0.00280 0.00003 -0.00274
.00408 0.00299 -0.00006 -0.00278
.00122 0.00187 -0.00004 -0.00215
.00474 0.00383 -0.00005 -0.00266
.02165 0.00465 -0.00005 -0.00382
:)
Z-
0
0
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0
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0
0
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0
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0
0
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0
0
-0
-0
-0
0
0
-0
0
0
0
0
-0
0
49


STAAD SPACE
************* ************************** **************
JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
140 0.00485 -0.11862 0.01221 0.00510 -0.00003 -0.00348
87 100 -0.00908 -0.05364 0.00330 -0.00080 0.00005 0.00181
110 -0.00799 -0.04254 0.00032 -0.00080 0.00003 0.00146
120 -0.00849 -0.05015 -0.00685 0.00048 0.00000 0.00126
130 -0.03249 -0.08685 -0.02042 -0.00170 0.00002 0.00301
140 -0.03257 -0.07291 -0.03067 -0.00025 -0.00005 0.00233
88 100 -0.00908 -0.09072 0.00426 -0.00247 0.00004 0.00227
110 -0.00801 -0.07289 0.00109 -0.00219 0.00003 0.00187
120 -0.00856 -0.07607 -0.00607 -0.00109 0.00005 0.00176
130 -0.02175 -0.14274 -0.02016 -0.00426 -0.00001 0.00333
140 -0.02188 -0.11833 -0.03088 -0.00268 -0.00001 0.00267
89 100 -0.00847 0.00000 0.00217 0.00063 -0.00015 -0.00167
110 -0.00743 0.00000 0.00036 0.00042 -0.00013 -0.00072
120 -0.00740 0.00000 -0.00286 0.00093 -0.00017 -0.00221
130 0.02700 0.00000 0.01567 0.00088 -0.00002 -0.00377
140 0.02759 0.00000 0.01010 0.00114 -0.00003 -0.00376
90 100 -0.00932 0.00000 0.00197 0.00075 0.00015 0.00278
110 -0.00807 0.00000 0.00034 0.00058 0.00012 0.00188
120 -0.00812 0.00000 -0.00297 0.00106 0.00014 0.00328
130 -0.04496 0.00000 0.01444 0.00055 0.00006 0.00428
140 -0.04415 0.00000 0.00958 0.00112 0.00002 0.00468
91 100 -0.00848 0.00000 0.00191 -0.00030 -0.00013 -0.00057
110 -0.00757 0.00000 0.00009 -0.00035 -0.00013 -0.00039
120 -0.00819 0.00000 -0.00317 0.00014 -0.00019 0.00008
130 0.02749 0.00000 -0.01491 -0.00044 -0.00004 -0.00255
140 0.02711 0.00000 -0.02047 -0.00003 -0.00009 -0.00172
92 100 -0.00968 0.00000 0.00175 -0.00065 0.00013 0.00213
110 -0.00841 0.00000 0.00009 -0.00060 0.00012 0.00171
120 -0.00873 0.00000 -0.00334 -0.00013 0.00016 0.00130
130 -0.04457 0.00000 -0.01610 -0.00092 0.00007 0.00423
140 -0.04414 0.00000 -0.02106 -0.00038 0.00008 0.00320
93 100 -0.01301 -0.00206 -0.00705 0.00074 -0.00046 -0.00070
110 -0.00919 -0.00544 -0.00494 0.00047 -0.00032 -0.00037
120 -0.01121 -0.00377 -0.00954 0.00039 -0.00058 -0.00047
130 0.00299 0.03108 -0.01150 0.00047 -0.00027 -0.00293
140 0.00650 0.02675 -0.01303 0.00001 -0.00033 -0.00247
94 100 0.00167 0.01206 -0.00705 0.00047 -0.00064 -0.00084
110 0.00089 0.00410 -0.00493 0.00030 -0.00045 -0.00043
120 0.00391 0.00311 -0.00948 0.00013 -0.00074 -0.00058
50


STAAD SPACE
JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
130 0.01095 0.04026 0.00280 0.00029 -0.00036 -0.00297
140 0.01293 0.02677 0.00134 -0.00014 -0.00037 -0.00243
95 100 0.00171 -0.00067 0.00002 0.00013 -0.00037 -0.00101
110 0.00092 -0.00257 0.00000 -0.00004 -0.00024 -0.00058
120 0.00392 -0.00595 -0.00006 -0.00031 -0.00050 -0.00078
130 0.00187 -0.00181 0.00713 0.00000 -0.00026 -0.00309
140 0.00381 -0.00778 0.00704 -0.00051 -0.00034 -0.00257
96 100 0.00000 0.00000 0.00000 -0.00013 -0.00008 -0.00101
110 0.00000 0.00000 0.00000 -0.00030 -0.00003 -0.00058
120 0.00000 0.00000 0.00000 -0.00063 -0.00031 -0.00078
130 0.00000 0.00000 0.00000 -0.00022 -0.00014 -0.00309
140 0.00000 0.00000 0.00000 -0.00078 -0.00035 -0.00257
97 100 0.00168 -0.01137 0.00530 0.00044 -0.00064 -0.00105
110 0.00089 -0.00903 0.00340 0.00028 -0.00043 -0.00064
120 0.00389 -0.01448 0.00536 0.00006 -0.00063 -0.00084
130 -0.00464 -0.03315 0.01036 0.00025 -0.00037 -0.00312
140 -0.00270 -0.03419 0.00968 -0.00020 -0.00027 -0.00264
98 100 -0.01315 -0.02234 0.00535 0.00030 -0.00050 -0.00073
110 -0.00931 -0.01713 0.00342 0.00021 -0.00033 -0.00042
120 -0.01133 -0.01743 0.00530 -0.00010 -0.00051 -0.00054
130 -0.01280 -0.04014 -0.00392 0.00018 -0.00029 -0.00292
140 -0.00925 -0.03188 -0.00470 -0.00024 -0.00023 -0.00249
99 100 -0.01302 -0.01337 -0.00002 0.00095 -0.00074 -0.00091
110 -0.00921 -0.01165 -0.00004 0.00079 -0.00051 -0.00054
120 -0.01123 -0.01094 -0.00010 0.00067 -0.00075 -0.00061
130 -0.00620 -0.01010 -0.00713 0.00069 -0.00040 -0.00299
140 -0.00270 -0.00679 -0.00720 0.00034 -0.00031 -0.00245
100 100 0.00000 0.00000 0.00000 0.00132 -0.00135 -0.00091
110 0.00000 0.00000 0.00000 0.00116 -0.00096 -0.00054
120 0.00000 0.00000 0.00000 0.00112 -0.00112 -0.00061
130 0.00000 0.00000 0.00000 0.00100 -0.00062 -0.00299
140 0.00000 0.00000 0.00000 0.00072 -0.00022 -0.00245
101 100 0.01259 -0.03801 0.00483 0.00033 0.00045 0.00221
110 0.00906 -0.03087 0.00319 0.00023 0.00031 0.00173
120 0.01063 -0.03138 0.00466 -0.00007 0.00045 0.00186
130 0.01152 -0.05298 -0.00509 0.00015 0.00019 0.00428
140 0.00846 -0.04559 -0.00542 -0.00024 0.00017 0.00385
102 100 -0.00115 -0.02640 0.00479 0.00045 0.00059 0.00251
110 -0.00065 -0.02225 0.00317 0.00030 0.00041 0.00195
51


STAAD SPACE
*****************************************************
JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
120 -0.00321 -0.02792 0.00472 0.00007 0.00057 0.00216
130 0.00582 -0.04756 0.00919 0.00015 0.00025 0.00443
140 0.00345 -0.04816 0.00897 -0.00023 0.00020 0.00398
103 100 -0.00118 -0.00108 0.00002 0.00011 0.00032 0.00247
110 -0.00067 -0.00268 0.00000 -0.00004 0.00022 0.00189
120 -0.00324 -0.00622 -0.00006 -0.00032 0.00044 0.00209
130 -0.00069 -0.00326 0.00713 -0.00013 0.00014 0.00437
140 -0.00306 -0.00848 0.00704 -0.00057 0.00027 0.00389
104 100 0.00000 0.00000 0.00000 -0.00017 0.00003 0.00247
110 0.00000 0.00000 0.00000 -0.00032 0.00001 0.00189
120 0.00000 0.00000 0.00000 -0.00066 0.00024 0.00209
130 0.00000 0.00000 0.00000 -0.00036 0.00003 0.00437
140 0.00000 0.00000 0.00000 -0.00085 0.00028 0.00389
105 100 -0.00114 0.03187 -0.00632 0.00047 0.00059 0.00229
110 -0.00065 0.02220 -0.00461 0.00031 0.00043 0.00172
120 -0.00323 0.02108 -0.00858 0.00013 0.00068 0.00188
130 -0.00977 0.05676 0.00447 0.00016 0.00024 0.00426
140 -0.01219 0.04446 0.00236 -0.00018 0.00030 0.00375
106 100 0.01246 0.01781 -0.00632 0.00072 0.00042 0.00216
110 0.00895 0.01240 -0.00462 0.00048 0.00030 0.00167
120 0.01052 0.01418 -0.00865 0.00037 0.00052 0.00178
130 -0.00424 0.05098 -0.00983 0.00027 0.00018 0.00427
140 -0.00727 0.04559 -0.01201 -0.00006 0.00026 0.00380
107 100 0.01246 -0.01413 -0.00002 0.00100 0.00069 0.00239
110 0.00896 -0.01218 -0.00004 0.00083 0.00048 0.00186
120 0.01054 -0.01153 -0.00010 0.00071 0.00068 0.00195
130 0.00493 -0.00921 -0.00713 0.00060 0.00028 0.00437
140 0.00192 -0.00686 -0.00720 0.00033 0.00024 0.00381
108 100 0.00000 0.00000 0.00000 0.00140 0.00130 0.00239
110 0.00000 0.00000 0.00000 0.00121 0.00094 0.00186
120 0.00000 0.00000 0.00000 0.00118 0.00106 0.00195
130 0.00000 0.00000 0.00000 0.00093 0.00051 0.00437
140 0.00000 0.00000 0.00000 0.00073 0.00015 0.00381
109 100 0.00182 0.02334 0.01052 0.00037 -0.00010 -0.00039
110 -0.00427 -0.00701 0.00000 0.00004 -0.00006 -0.00016
120 0.00426 0.06809 0.02338 0.00111 -0.00006 -0.00043
130 0.06441 0.03892 0.05584 0.00049 -0.00009 -0.00104
140 0.05967 0.07275 0.06491 0.00110 0.00001 -0.00082
110 100 0.00182 0.01910 0.01856 0.00041 -0.00013 -0.00041
52


STAAD SPACE
*****************************************************
JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
110 -0.00427 -0.00492 0.00509 0.00006 -0.00009 -0.00015
120 0.00425 0.06435 0.03082 0.00123 -0.00015 -0.00049
130 0.03254 0.01970 0.06782 0.00068 -0.00025 -0.00117
140 0.02780 0.06190 0.07262 0.00128 -0.00020 -0.00095
111 100 0.00183 0.01467 0.01948 0.00063 0.00003 -0.00040
110 -0.00426 -0.00457 0.00629 0.00019 0.00001 -0.00013
120 0.00425 0.06085 0.03495 0.00148 -0.00003 -0.00048
130 -0.00452 -0.01442 0.07409 0.00122 -0.00006 -0.00121
140 -0.00925 0.04741 0.07930 0.00170 -0.00009 -0.00097
112 100 -0.03216 0.02675 0.00424 0.00012 -0.00016 0.00118
110 -0.02455 0.00566 -0.00217 -0.00006 -0.00011 0.00083
120 -0.03522 0.07498 0.01948 0.00093 -0.00011 0.00129
130 -0.09855 0.00862 0.03683 -0.00027 -0.00028 0.00220
140 -0.09813 0.06793 0.05594 0.00074 -0.00025 0.00216
113 100 -0.03154 0.00737 0.00366 0.00017 0.00009 0.00092
110 -0.02508 0.00938 -0.00093 -0.00004 0.00012 0.00069
120 -0.02315 -0.05262 0.02490 0.00085 0.00044 0.00058
130 -0.09630 0.03301 -0.04858 -0.00015 0.00007 0.00163
140 -0.08478 -0.03702 -0.02296 0.00068 0.00041 0.00115
114 100 -0.03153 -0.01260 0.00362 0.00013 -0.00005 0.00102
110 -0.02508 -0.00604 0.00216 0.00009 0.00003 0.00078
120 -0.02315 -0.06998 0.04736 0.00183 0.00045 0.00065
130 -0.06443 -0.00068 -0.05401 -0.00022 -0.00020 0.00191
140 -0.05291 -0.06283 -0.00638 0.00164 0.00029 0.00138
115 100 -0.00907 -0.01609 0.00616 0.00022 0.00010 0.00002
110 -0.00948 -0.00772 0.00391 0.00014 -0.00004 0.00008
120 -0.01249 -0.07300 0.05557 0.00219 -0.00050 0.00015
130 0.01058 -0.01777 -0.04324 0.00023 0.00035 -0.00070
140 0.00422 -0.06852 0.00453 0.00211 -0.00030 -0.00034
116 100 -0.00908 -0.02805 0.01010 0.00043 0.00001 -0.00002
110 -0.00949 -0.01548 0.00150 0.00006 -0.00005 0.00004
120 -0.01251 -0.08151 0.02888 0.00102 -0.00041 0.00010
130 0.04769 -0.03082 -0.02851 0.00058 0.00005 -0.00034
140 0.04128 -0.07740 -0.01360 0.00104 -0.00037 -0.00019
117 100 0.01006 0.02333 0.01678 0.00034 0.00008 -0.00050
110 -0.00098 -0.00702 0.00038 0.00000 0.00004 -0.00022
120 0.01393 0.06809 0.04294 0.00108 0.00014 -0.00057
130 0.08719 0.02722 0.06404 0.00044 0.00029 -0.00126
140 0.07826 0.06105 0.08424 0.00107 0.00038 -0.00104
53


301NT DI^PLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
I
I
I
1
I
I
I
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H- o o o o o o o O o o O o O O O O o O O O o o o o O O o O o O o o o o O O o o o
o zc o o o o O o o o o o O o O o o o O o o o o O O o o o o o o o o o O o 3 o
i ivj o 0 1 0 1 0 1 0 1 0 1 o O 1 0 1 o \ o o o O o o o o o O o o o o o o o o o o o o o o o o o O 0 1
m o 00 CM CM O' 00 o 00 o ro 00 n* M) ro o O' o O' r*^ o ro ro m CM o M* O'
2 CM H CM K) o o o iH H CM CM H ro ro CM H M ro CM H ro ro ro CM n- 00 H O n* ro m CM O m
t o O o o O o o o o o o o o o o o o o o o O o o o O o o o o o o o o o o o O o o
O or o o o o O o o o o o o o o o o o o o o o O o o o O o o o o o o o o o o o o o o
>- 0 1 0 1 0 1 0 1 O 1 0 1 0 1 0 1 0 1 o 0 1 0 1 0 1 0 1 0 1 0 1 0 1 0 1 0 1 o o o o o O o o o o o 0 1 o o 0 1 o o 0 1 0 1 o
in CM >o n* M) o r^ in ro o CO H o CM ro o o CM H sO o O' O' ro CM H 00 o o ro O' o O' ro 00 O'
2 *o o m H vO *-4 -4- 1 H o o ro h- CM o o o 00 H o 00 CM sO H o 00 H 'O CM M3 o m CM H o ro
i o o o o o o o O o O o o o o o o o o o O O o o o o O o o o o O o O C3 O O O o o
0 EC 1 X o o o o o o o o o o o o o o o o o o o O O o o o o O o o o o O o o o o O o o o
o o o o o o o o o o o 0 1 o 0 1 o o o o 0 1 o O 0 1 o 0 1 o o 0 1 o 0 1 o O o o 0 1 o o o o O
CO *0 in o 00 %o m m CM H -* m ro 00 H * m CM 00 O n- o vO o 00 sO NO 00 m 1 03 o o O' o in 00 CM
CO o md O' M o M3 m K3 JO CM H ro o H r- ro o ro O' O m o 00 o >o n* O' 00 O' ro 00 O' ro CO CM
2 m m H 00 o O' H in O M5 ro M3 H 00 M) ro o o n* H 00 O' CO SO H 00 o NO ro 00 M) H o M> CM I-*-
a: o o o o o o o o O o o o o o o o O o o o o o o o o O o o o o o o O o o o o
M o o o o o o o o o o O 0 1 o o o o 0 1 o o o o 0 1 o 0 1 o o 0 1 O 0 1 0 1 o o o 0 1 O o o o o
00 ro 00 00 NO 00 M1 fO o m in n- 00 CM CM o m H ro m H m o O' NO r^ CM H CM m O' o m o ro 1 00
c m 00 H 'O O' o CM ro CM ao o CM X* m ro ro sO ro n* M5 o O' m t4 n- o "t
M" O NO m M3 m ro sO o vO n- ro H CM 00 ro r^ O' CM H 00 CM o o CM M- M3 ro O'
CC o 3 O O o o O o o o o o o o o O o O o o O O O o O o a o O o O O o O o O o o O
1 >- o T O O o o O 1 o 0 1 o o o o 0 1 o o o O o o O o 0 1 o o o o 0 1 o 0 1 0 1 0 1 0 1 0 1 o O 1 0 1 0 1 0 1
-< M M> M* o r- CM < o CM 00 00 H m 00 ro 00 o o o M ro o o O' O' 00 n* M> 'C n* M> O CM m n*
CO o O 00 CM K) O' o 00 H CM n M- 00 o ro 00 m o o NO in 00 n- ro rH 00 MD ro ro H O' 't CM CM
2 o ro m vC O' * 1 m 00 o -4- o 00 o 00 ro in o ro o ro r^ o o m o O' o O' m 00 n- 00 O
o < m m ro m ro ro ro o m ro ro O' n- o H H CM
cd o o O o o o o o O o o O o H H o o o H H o o o H H o o o H H o o o O o o O O O
i X o o o o o o 0 1 c o o 0 1 0 1 0 1 o O 1 0 1 0 1 0 1 O 1 O 1 0 1 0 1 0 1 O t 0 1 0 1 0 1 0 1 O 1 0 1 0 1 0 1 0 1 O f 0 1 0 1 o 0 1 O
3 o O O O O O 3 O o O 3 O O O O o o O O o o O O o O O o O O O O O O O O O O O O
a CJ CM ro o CM ro M- O H CM ro M- o H CM r*3 o H CM ro M* O H CM ro M- O H CM ro o H CM ro
O H i H H -1 *1 4 H H * i H H H H H H H H H H i H H H H *4 H H H H H H
1 00 O' o H CM ro M- m
2 < H CM CM CM CM CM CM
M o *-) 1 > 1 f 4 4 H H H
in


STAAD SPACE
I*****************************************************
JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS Z-TRANS X-ROTAN Y-ROTAN Z-ROTAN
140 0.01016 -0.08023 0.04113 0.00196 -0.00051 -0.00005
126 100 -0.00867 -0.02806 0.01799 0.00045 -0.00010 -0.00008
110 -0.01040 -0.01548 0.00243 0.00007 -0.00012 -0.00002
120 -0.01423 -0.08150 0.04585 0.00101 -0.00065 -0.00006
130 0.05837 -0.04253 -0.01750 0.00063 -0.00028 -0.00059
140 0.04725 -0.08909 0.00380 0.00104 -0.00079 -0.00043
127 100 -0.00031 -0.01198 0.01800 0.00032 -0.00033 -0.00015
110 -0.00528 -0.00896 0.00242 0.00000 -0.00016 -0.00004
120 0.00325 -0.03487 0.04578 0.00098 -0.00043 -0.00030
130 0.07988 -0.01978 0.00332 0.00045 -0.00072 -0.00078
140 0.07472 -0.04149 0.02454 0.00096 -0.00075 -0.00079
128 100 0.01536 0.01308 0.01676 0.00044 -0.00005 -0.00075
110 0.00186 -0.00491 0.00037 0.00011 -0.00003 -0.00039
120 0.02155 0.03420 0.04292 0.00114 -0.00003 -0.00088
130 0.10423 0.01347 0.04320 0.00056 0.00016 -0.00179
140 0.09724 0.02721 0.06341 0.00114 0.00018 -0.00157
129 100 0.01538 -0.04614 0.03025 0.00030 -0.00055 -0.00130
110 0.00187 -0.03836 0.00894 -0.00001 -0.00035 -0.00064
120 0.02158 -0.03623 0.05672 0.00105 -0.00057 -0.00160
130 0.08315 -0.11225 0.05869 0.00031 -0.00072 -0.00315
140 0.07616 -0.08551 0.07809 0.00094 -0.00069 -0.00279
130 100 -0.06361 -0.05363 0.00152 0.00031 -0.00033 0.00180
110 -0.04987 -0.04253 -0.00763 0.00009 -0.00031 0.00141
120 -0.05445 -0.05016 0.03762 0.00125 -0.00019 0.00109
130 -0.13233 -0.11459 -0.03926 0.00013 -0.00056 0.00361
140 -0.11659 -0.10068 0.00382 0.00124 -0.00043 0.00246
131 100 -0.00343 -0.09914 0.00080 0.00020 0.00002 0.00160
110 -0.00245 -0.10504 0.00289 -0.00025 -0.00002 0.00184
120 -0.00275 -0.06273 -0.02038 0.00100 -0.00001 0.00156
130 -0.02489 -0.05623 0.01932 -0.00002 -0.00008 0.00142
140 -0.02099 -0.03381 -0.00079 0.00089 -0.00005 0.00155
132 100 -0.00358 -0.09321 -0.00165 0.00034 -0.00011 -0.00135
110 -0.00252 -0.13420 0.00036 -0.00005 -0.00005 -0.00113
120 -0.00296 -0.06878 -0.02292 0.00114 -0.00008 -0.00117
130 0.00537 -0.05575 0.01484 0.00026 -0.00010 -0.00139
140 0.00923 -0.03804 -0.00406 0.00108 -0.00007 -0.00126
133 100 -0.00290 -0.12301 -0.00978 0.00037 0.00003 -0.00135
110 -0.00281 -0.07526 -0.02756 0.00234 0.00018 -0.00081
120 -0.00108 0.01034 -0.13067 0.01187 0.00069 0.00062
55


STAAD SPACE
*****************************************************
JOINT DISPLACEMENT (INCH RADIANS) STRUCTURE TYPE = SPACE
JOINT LOAD X-TRANS Y-TRANS
130 0.01687 -0.06946
140 0.01651 0.04601
134 100 -0.00281 -0.10539
110 -0.00274 -0.06340
120 -0.00105 0.01337
130 -0.01342 -0.04912
140 -0.01386 0.05058
135 100 -0.00763 -0.03013
110 -0.00682 -0.02144
120 -0.00682 -0.03085
130 0.02093 -0.05488
140 0.02107 -0.05039
136 100 -0.00558 -0.02247
110 -0.00533 -0.01725
120 -0.00583 -0.01756
130 0.02196 -0.04802
140 0.02070 -0.03976
137 100 -0.01019 -0.04407
110 -0.00872 -0.03447
120 -0.00888 -0.04363
130 -0.03856 -0.06325
140 -0.03758 -0.06206
138 100 -0.01241 -0.03815
110 -0.01043 -0.03100
120 -0.01052 -0.03152
130 -0.03920 -0.06087
140 -0.03744 -0.05348
Z-TRANS X-ROTAN Y-ROTAN
-0.02839 0.00041 -0.00007
-0.15003 0.01184 0.00066
-0.00755 0.00021 -0.00012
-0.02657 0.00220 -0.00022
-0.13023 0.01166 -0.00071
-0.02404 0.00013 -0.00013
-0.14892 0.01157 -0.00071
0.00327 0.00017 0.00006
0.00130 0.00025 0.00004
-0.00169 0.00002 0.00001
0.00781 0.00031 0.00004
0.00222 0.00025 -0.00002
0.00340 -0.00046 -0.00016
0.00142 -0.00037 -0.00013
-0.00152 -0.00074 -0.00017
-0.00646 -0.00057 -0.00006
-0.01201 -0.00082 -0.00005
0.00306 0.00026 -0.00006
0.00120 0.00030 -0.00004
-0.00212 0.00009 -0.00004
0.00693 0.00041 -0.00001
0.00163 0.00032 0.00002
0.00315 -0.00044 0.00015
0.00129 -0.00038 0.00011
-0.00198 -0.00073 0.00013
-0.00735 -0.00046 0.00007
-0.01261 -0.00079 0.00003
************** end OF LATEST ANALYSIS RESULT **************
463. PAGE NEW
Z-ROTAN
-0.00106
0.00062
0.00155
0.00097
-0.00023
0.00156
-0.00014
-0.00181
-0.00109
-0.00187
-0.00402
-0.00358
-0.00096
-0.00058
-0.00072
-0.00320
-0.00267
0.00307
0.00227
0.00303
0.00490
0.00468
0.00237
0.00185
0.00199
0.00446
0.00396
56


STAAD SPACE
*****************************************************
464. ******************************
465. ****MEMBER FORCES*************
466. ******************************
467. PRINT MEMBER FORCES
57


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
MEMB LOAD JT AXIAL SHEAR-Y
1 100 1 -42.90 55.91
2 42.90 27.80
110 1 -64.58 117.21
2 64.58 -45.46
120 1 -45.81 69.47
2 45.81 2.28
130 1 -45.90 69.70
2 45.90 2.06
140 1 -46.24 69.45
2 46.24 2.30
2 100 2 -56.74 -74.54
3 56.74 83.17
110 2 -74.23 -326.31
3 74.23 333.70
120 2 -57.00 -145.46
3 57.00 152.86
130 2 -55.18 -145.90
3 55.18 153.29
140 2 -56.88 -145.19
3 56.38 152.59
3 100 3 -45.78 78.76
4 45.78 -68.96
110 3 -22.94 99.05
4 22.94 -90.64
120 3 -35.27 76.82
4 35.27 -68.42
130 3 -42.68 77.16
4 42.68 -68.75
140 3 -39.00 76.41
4 39.00 -68.00
4 100 4 -37.04 22.29
5 37.04 56.08
110 4 -23.69 24.49
5 23.69 42.68
120 4 -29.90 20.91
5 29.90 46.26
SHEAR-Z TORSION MOM-Y MOM-Z
8.51 -242.79 -203.69 460.11
-8.51 242.79 -196.33 200.51
2.39 116.33 -68.87 1587.58
-2.39 -116.33 -43.40 2235.08
5.78 -101.53 -141.13 765.60
-5.78 101.53 -130.37 813.24
4.71 -72.25 -110.27 769.28
-4.71 72.25 -111.29 820.26
5.46 -86.44 -130.98 765.36
-5.46 86.44 -125.62 812.50
7.30 364.13 -43.24 -645.10
-7.30 -364.13 -117.30 -1089.73
10.75 -348.34 -125.56 -3371.17
-10.75 348.34 -110.95 -3888.90
7.83 103.73 -64.25 -1429.34
-7.83 -103.73 -108.08 -1852.13
6.38 144.01 -49.67 -1429.96
-6.38 -144.01 -90.65 -1861.11
7.58 115.92 -59.80 -1425.48
-7.58 -115.92 -107.05 -1850.14
-7.90 -305.45 171.62 1112.27
7.90 305.45 25.88 734.21
3.21 -584.20 5.51 1788.78
-3.21 584.20 -85.85 582.33
-3.97 -360.57 106.86 1208.24
3.97 360.57 -7.67 607.20
-7.40 -334.00 161.78 1213.35
7.40 334.00 23.29 610.49
-5.48 -350.48 130.50 1204.11
5.48 350.48 6.53 601.04
-6.52 303.75 135.19 -311.94
6.52 -303.75 151.64 -431.49
-2.69 321.42 70.79 -152.88
2.69 -321.42 47.70 -247.13
-4.83 272.70 105.34 -228.50
4.83 -272.70 107.06 -329.31
58


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE -- POUN INCH
MEMB LOAD JT AXIAL SHEAR-Y
130 4 -33.13 21.55
5 33.13 45.62
140 4 -31.76 21.23
5 31.76 45.94
5 100 1 -2.93 -11.66
6 2.93 24.21
110 1 0.15 4.87
6 -0.15 5.89
120 1 -1.09 -5.52
6 1.09 16.28
130 1 -0.56 -2.31
6 0.56 13.07
140 1 -0.46 -4.52
6 0.46 15.28
6 100 6 -16.63 67.61
7 16.63 16.10
110 6 -41.16 71.67
7 41.16 0.08
120 6 -21.93 61.83
7 21.93 9.92
130 6 -19.41 59.74
7 19.41 12.01
140 6 -20.29 60.71
7 20.29 11.04
7 100 7 -8.82 12.38
8 8.82 -3.76
110 7 -25.60 6.80
8 25.60 0.60
120 7 -11.70 9.22
8 11.70 -1.82
130 7 -7.08 7.76
8 7.08 -0.37
140 7 -8.46 8.51
8 8.46 -1.12
8 100 8 -8.83 3.76
9 8.83 6.05
110 8 -25.60 -0.60
9 25.60 9.00
SHEAR-Z TORSION MOM-Y MOM-Z
-6.97 296.90 148.28 -214.88
6.97 -296.90 158.62 -314.46
-5.71 273.76 123.81 -221.31
' 5.71 -273.76 127.30 -322.34
-15.57 130.64 245.21 -262.29
15.57 -130.64 253.01 -311.63
-6.51 -211.71 96.76 22.61
6.51 211.71 111.62 -38.84
-11.60 11.01 181.51 -150.97
11.60 -11.01 189.62 -197.80
H i 1 8.01 186.47 -100.52
11.71 -8.01 188.24 -145.55
-12.08 10.01 190.90 -135.77
12.08 -10.01 195.55 -181.03
9.74 -124.14 -217.69 815.09
-9.74 124.14 -240.23 395.49
2.98 39.09 -67.74 860.88
-2.98 -39.09 -72.17 821.52
6.77 -59.83 -151.05 740.40
-6.77 59.83 -167.03 479.67
5.73 -32.90 -124.37 688.58
-5.73 32.90 -144.37 432.93
6.55 -49.27 -144.83 713.63
-6.55 49.27 -163.15 453.49
0.41 1.71 19.82 112.08
-0.41 -1.71 -28.73 65.46
4.84 -219.38 -100.84 63.46
-4.84 219.38 -5.72 4.76
1.66 -68.16 -17.00 82.45
-1.66 68.16 -19.55 38.94
0.56 -39.21 11.90 48.07
-0.56 39.21 -24.24 41.35
1.22 -58.90 -4.82 67.42
-1.22 58.90 -22.06 38.48
0.41 1.71 28.73 -65.46
-0.41 -1.71 -38.87 36.77
4.84 -219.38 5.73 -4.76
-4.84 219.38 -126.83 -115.24
59


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM
120 8 -11.71 1.82 1.66 -68.16 19.55 -38.
9 11.71 6.59 -1.66 68.16 -61.08 -20.
130 8 -7.08 0.37 .0.56 -39.21 24.24 -41.
9 7.08 8.04 -0.56 39.21 -38.26 -54.
140 8 -8.47 1.12 1.22 -58.90 22.06 -38.
9 8.47 7.29 -1.22 58.90 -52.61 -38.
100 9 -10.63 4.60 -7.19 180.69 175.87 -641.
10 10.63 73.77 7.19 -180.69 140.27 -880.
110 9 -11.79 2.58 -2.01 156.84 56.72 -579.
10 11.79 64.59 2.01 -156.84 31.52 -785.
120 9 -8.79 3.99 -5.01 153.47 125.34 -549.
10 8.79 63.18 5.01 -153.47 95.08 -752.
130 9 -5.81 2.18 -7.76 179.12 186.99 -590.
10 5.81 64.99 7.76 -179.12 154.50 -791.
140 9 -6.46 3.91 -6.12 159.40 151.07 -552.
10 6.46 63.26 6.12 -159.40 118.35 -752.
100 5 -4.16 -12.88 10.86 -204.02 -159.14 -280.
10 4.16 25.44 -10.86 204.02 -188.23 -332.
110 5 -4.52 -7.58 5.22 -224.09 -79.12 -189.
10 4.52 18.34 -5.22 224.09 -87.92 -225.
120 5 -3.43 -10.22 8.73 -191.24 -129.54 -229.
10 3.43 20.98 -8.73 191.24 -149.82 -270.
130 5 -3.96 -15.54 12.04 -209.85 -181.88 -312.
10 3.96 26.30 -12.04 209.85 -203.44 -357.
140 5 -3.21 -12.11 10.64 -198.49 -159.89 -259.
10 3.21 22.87 -10.64 198.49 -180.67 -300.
100 11 -10.41 73.66 -7.27 185.00 140.28 879.
12 10.41 4.71 7.27 -185.00 179.79 637.
110 11 -30.89 54.39 10.67 97.71 -252.40 565.
12 30.89 12.78 -10.67 -97.71 -216.90 349.
120 11 -112.80 23.81 71.89 -106.71 -1600.86 -88.
12 112.80 43.36 -71.89 106.71 -1562.51 -341.
130 11 -5.76 64.47 -8.86 179.96 176.55 782.
12 5.76 2.70 8.86 -179.96 213.22 576.
140 11 -110.78 23.79 70.87 -102.48 -1579.90 -89.
12 110.78 43.38 -70.87 102.48 -1538.36 -341.
100 12 -9.01 6.33 0.54 6.81 -41.80 -30.
13 9.01 3.48 -0.54 -6.81 28.40 65.
l-Z
94
64
35
55
48
70
73
08
05
10
65
51
60
29
93
61
33
78
29
33
03
19
23
13
11
67
21
81
81
65
53
67
85
15
33
73
05
68
60


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y
110 12 -41.42 5.81 0.59 -5.93 36.21
13 41.42 2.59 -0.59 5.93 -51.06
120 12 -166.22 8.31 0.10 -26.46 327.86
13 166.22 0.10 -0.10 26.46 -330.42
130 12 -2.62 6.97 -0.73 33.89 -10.80
13 2.62 1.43 0.73 -33.89 29.03
140 12 -163.31 9.02 -0.33 -16.14 336.49
13 163.31 -0.62 0.33 16.14 -328.30
100 13 -9.01 -3.48 0.54 6.81 -28.40
14 9.01 12.11 -0.54 -6.81 16.61
110 13 -41.43 -2.59 0.59 -5.92 51.06
14 41.43 9.99 -0.59 5.92 -64.11
120 13 -166.22 -0.10 0.11 -26.46 330.39
14 166.22 7.50 -0.11 26.46 -332.73
130 13 -2.62 -1.43 -0.73 33.89 -29.03
14 2.62 8.83 0.73 -33.89 45.09
140 13 -163.31 0.62 -0.32 -16.14 328.28
14 163.31 6.78 0.32 16.14 -321.16
100 14 -16.77 15.78 9.76 -126.11 -238.71
15 16.77 67.92 -9.76 126.11 -219.88
110 14 -36.14 19.19 -6.39 -55.87 139.02
15 36.14 52.56 6.39 55.87 161.27
120 14 -116.66 41.83 -62.85 162.64 1452.91
15 116.66 29.92 62.85 -162.64 1501.21
130 14 -11.65 15.99 7.20 -78.16 -179.91
15 11.65 55.76 -7.20 78.16 -158.40
140 14 -115.26 43.02 -63.21 175.39 1460.15
15 115.26 28.73 63.21 -175.39 1510.75
100 11 -3.77 25.36 11.23 -207.06 -194.84
16 3.77 -12.81 -11.23 207.06 -164.61
110 11 14.35 -38.63 -14.91 -80.88 192.22
16 -14.35 49.39 14.91 80.38 284.89
120 11 79.08 -260.36 -105.28 270.07 1512.75
16 -79.08 271.12 105.28 -270.07 1856.08
130 11 -3.57 26.82 13.02 -193.91 -223.18
16 3.57 -16.06 -13.02 193.91 -193.58
140 11 78.92 -253.55 -103.50 264.01 1483.17
16 -78.92 269.31 103.50 -264.01 1828.88
MOM-Z
25.28
15.03
238.07
-135.48
12.30
56.99
256.98
-136.44
-65.68
-105.74
-15.03
-123.32
135.48
-219.03
-57.00
-55.84
136.45
-204.18
-405.08
-820.18
-220.84
-563.25
283.89
-3.79
-291.10
-643.53
311.64
24.15
331.15
279.58
-693.70
-714.64
-4283.04
-4220.66
366.51
319.69
-4253.38
-4192.38
61


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
MEMB LOAD JT AXIAL SHEAR-Y
16 100 16 -37.94 56.04
17 37.94 22.32
110 16 -8.74 53.57
17 8.74 13.60
120 16 79.06 73.88
17 -79.06 -6.71
130 16 -35.78 47.31
17 35.78 19.86
140 16 77.31 73.53
17 -77.31 -6.36
17 100 17 -46.47 -68.89
18 46.47 78.70
110 17 0.28 -70.95
18 -0.28 79.35
120 17 146.07 -116.05
18 -146.07 124.46
130 17 -47.35 -59.03
18 47.35 67.44
140 17 142.60 -115.57
18 -142.60 123.97
18 100 18 -56.39 83.47
19 56.39 -74.84
110 18 -7.71 86.81
19 7.71 -79.41
120 18 147.15 144.51
19 -147.15 -137.11
130 18 -46.28 71.72
19 46.28 -64.33
140 18 147.61 144.18
19 -147.61 -136.78
19 100 19 -42.27 27.73
20 42.27 55.98
110 19 -11.35 18.86
20 11.35 52.89
120 19 82.23 0.15
20 -82.23 71.60
130 19 -36.33 23.62
20 36.33 48.13
SHEAR-Z TORSION MOM-Y MOM-Z
-6.52 304.85 151.15 432.38
6.52 -304.85 135.56 309.53
31.77 265.76 -332.64 476.38
12.45 -265.76 -92.42 403.06
169.72 310.02 -2019.43 862.77
39.63 -310.02 -842.48 910.11
-7.76 281.15 182.07 355.05
7.76 -281.15 159.51 248.75
168.85 311.97 -1998.95 855.98
40.51 -311.97 -824.54 901.53
-8.20 -303.96 23.64 -734.38
8.20 303.96 181.30 -1110.48
8.34 -489.73 -16.01 -746.32
16.29 489.73 109.20 -1132.40
65.94 -1322.42 -128.76 -1192.03
53.01 1322.42 -32.93 -1814.33
-10.32 -230.83 51.84 -627.09
10.32 230.83 206.20 -953.76
64.55 -1309.04 -116.17 -1184.85
54.40 1309.04 -10.76 -1809.46
7.28 373.24 -111.15 1094.75
-7.28 -373.24 -49.00 646.67
13.20 573.54 -55.92 1143.54
8.91 -573.54 8.66 684.95
37.25 1553.59 114.24 1919.68
67.42 -1553.59 217.68 1178.10
4.65 355.78 -78.24 945.16
-4.65 -355.78 -24.12 551.35
36.85 1563.73 118.12 1917.62
67.82 -1563.73 222.57 1172.94
8.42 -240.85 -194.27 -204.28
-8.42 240.85 -201.66 -459.69
17.19 -225.60 9.46 -314.20
30.04 225.60 292.47 -485.46
53.28 -278.44 689.56 -844.85
170.35 278.44 2061.64 -834.24
6.13 -175.34 -146.98 -179.30
-6.13 175.34 -141.34 -396.67
62


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE -- poun : [NCH
MEMB LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM
140 19 82.04 0.17 52.91 -263.69 695.77 -843.
20 -82.04 71.58 170.71 263.69 2072.45 -834.
20 100 15 -2.28 24.21 -15.35 129.06 247.57 310.
20 2.28 -11.66 15.35 -129.06 243.68 263.
110 15 15.94 -38.09 12.09 34.91 -153.38 -685.
20 -15.94 48.84 -12.09 -34.91 -233.51 -705.
120 15 82.73 -261.59 107.25 -252.06 -1533.19 -4302.
20 -82.73 272.35 -107.25 252.06 -1898.77 -4240.
130 15 -1.44 17.36 -13.31 107.03 212.67 210.
20 1.44 -6.60 13.31 -107.03 213.26 172.
140 15 82.86 -262.72 106.98 -254.09 -1529.71 -4320.
20 -82.86 273.48 -106.98 254.09 -1893.52 -4258.
21 100 2 1.21 46.74 -13.85 444.59 239.58 606.
7 -1.21 -34.19 13.85 -444.59 203.47 688.
110 2 -8.36 -28.24 -9.65 1136.09 168.96 -464.
7 8.36 38.99 9.65 -1136.09 139.91 -611.
120 2 -2.06 18.18 -11.19 616.10 194.61 205.
7 2.06 -7.42 11.19 -616.10 163.45 204.
130 2 -1.67 18.84 -9.27 609.69 160.96 216.
7 1.67 -8.08 9.27 -609.69 135.59 214.
140 2 -2.13 17.89 -10.65 612.98 185.42 202.
7 2.13 -7.13 10.65 -612.98 155.30 197.
22 100 4 -1.38 46.67 8.74 -422.27 -161.07 609.
9 1.38 -34.12 -8.74 422.27 -118.61 683.
110 4 5.90 66.15 -0.76 -429.46 15.06 905.
9 -5.90 -55.39 0.76 429.46 9.16 1038.
120 4 0.86 47.51 5.36 -378.70 -97.67 633.
9 -0.86 -36.75 -5.36 378.70 -73.98 714.
130 4 -0.43 47.20 9.56 -395.61 -171.57 630.
9 0.43 -36.44 -9.56 395.61 -134.24 707.
140 4 0.22 46.77 7.24 -379.72 -130.33 624.
9 -0.22 -36.02 -7.24 379.72 -101.31 700.
23 100 12 -1.68 -34.02 8.53 -424.85 -113.68 -680.
17 1.68 46.57 -8.53 424.85 -159.20 -608.
110 12 21.28 -46.59 -9.02 -343.26 180.18 -907.
17 -21.28 57.35 9.02 343.26 108.45 -755.
120 12 105.53 -112.00 -67.02 -281.92 1173.29 -2123.
17 -105.53 122.76 67.02 281.92 971.23 -1632.
i-Z
85
13
71
18
80
09
28
66
96
29
45
67
92
01
67
03
25
27
26
50
37
97
19
40
63
96
28
83
91
23
24
38
60
82
51
49
72
44
63


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE ~ POUN INCH
MEMB LOAD JT AXIAL SHEAR-Y
130 12 -2.55 -28.41
17 2.55 39.17
140 12 105.02 -111.17
17 -105.02 121.93
24 100 14 1.14 -34.56
19 -1.14 47.11
110 14 26.11 -49.80
19 -26.11 60.55
120 14 120.74 -126.20
19 -120.74 136.96
130 14 1.48 -29.95
19 -1.48 40.70
140 14 120.78 -125.85
19 -120.78 136.61
25 100 3 -241.17 14.57
21 255.29 12.50
110 3 -953.97 0.78
21 966.08 22.42
120 3 -439.73 8.85
21 451.83 14.35
130 3 -445.82 8.86
21 457.93 14.34
140 3 -441.30 8.87
21 453.40 14.33
26 100 3 42.09 0.81
22 -27.97 -0.81
110 3 32.99 37.38
22 -20.89 -37.38
120 3 35.18 12.17
22 -23.07 -12.17
130 3 35.17 12.31
22 -23.06 -12.31
140 3 35.23 12.23
22 -23.13 -12.23
27 100 3 -253.29 13.29
23 267.41 13.77
110 3 -959.16 20.88
23 971.27 2.31
SHEAR-Z TORSION MOM-Y MOM-Z
11.59 -378.34 -159.52 -569.30
-11.59 378.34 -211.35 -511.98
-65.28 -283.32 1148.26 -2108.55
65.28 283.32 940.70 -1621.01
-14.12 442.39 208.67 -692.71
14.12 -442.39 243.27 -614.09
3.64 370.75 -98.44 -966.44
-3.64 -370.75 -18.13 -799.14
64.92 333.25 -1170.26 -2378.55
-64.92 -333.25 -907.26 -1832.03
-9.95 372.05 147.20 -599.30
9.95 -372.05 171.10 -531.13
65.56 329.10 -1179.71 -2371.91
-65.56 -329.10 -918.35 -1827.42
-2.58 -66.11 116.63 200.31
2.58 66.11 83.93 -119.67
-2.66 -18.84 105.08 -413.38
2.66 18.84 101.96 -428.49
-2.53 -44.74 99.84 -10.29
2.53 44.74 97.41 -203.66
-3.14 -29.79 66.98 -9.42
3.14 29.79 177.62 -204.07
-2.93 -39.42 86.98 -9.24
2.93 39.42 141.19 -203.14
9.74 -14.14 -402.52 10.19
-9.74 14.14 52.01 18.88
3.99 13.59 -144.31 1035.26
-3.99 -13.59 0.60 310.59
7.09 -3.73 -281.23 329.94
-7.09 3.73 26.13 108.29
7.73 -24.21 -292.13 332.99
-7.73 24.21 13.97 110.03
7.44 -10.42 -284.86 331.35
-7.44 10.42 16.85 108.97
2.88 84.71 -171.64 167.58
-2.88 -84.71 -52.82 -186.37
0.88 26.68 -5.58 651.48
-0.88 -26.68 -63.29 71.17
64


STAAD SPACE
********************************
*********************
MEMBER END FORCES STRUCTURE TYPE = SPACE
UNITS ARE poun : INCH
LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y
120 3 -447.62 14.39 2.18 57.10 -100.72
23 459.72 8.31 -2.18 -57.10 -68.85
130 3 -443.14 14.37 2.91 71.12 -141.47
23 455.24 8.83 -2.91 -71.12 -85.17
140 3 -444.78 14.41 2.69 61.03 -112.96
23 456.88 8.79 -2.69 -61.03 -96.27
100 21 22.09 12.46 -4.58 -11.09 195.83
22 -22.09 14.60 4.58 11.09 120.08
110 21 742.76 9.11 -2.04 -0.35 102.81
22 -742.76 14.09 2.04 0.35 38.26
120 21 183.36 10.16 -3.40 -4.96 158.97
22 -183.36 13.04 3.40 4.96 75.82
130 21 -25.37 10.12 -3.36 24.57 177.23
22 25.37 13.08 3.36 -24.57 54.95
140 21 56.23 10.12 -3.44 7.01 176.16
22 -56.23 13.08 3.44 -7.01 61.43
100 22 21.28 13.37 5.16 40.92 -134.22
23 -21.28 13.70 -5.16 -40.92 -221.70
110 22 705.38 6.80 1.95 0.25 -24.67
23 -705.38 16.40 -1.95 -0.25 -109.71
120 22 171.19 10.04 3.68 21.17 -79.54
23 -171.19 13.16 -3.68 -21.17 -174.62
130 22 -37.68 9.98 4.36 38.54 -79.16
23 37.68 13.21 -4.36 -38.54 -221.80
140 22 44.00 10.05 4.00 23.86 -71.84
23 -44.00 13.15 -4.00 -23.86 -204.26
100 1 -44.26 -27.33 -5.58 -41.53 19.51
21 58.38 27.33 5.58 41.53 181.25
110 1 -122.09 -58.06 -2.53 -27.89 93.72
21 134.19 58.06 2.53 27.89 -2.71
120 1 -63.94 -34.21 -4.66 -40.39 49.44
21 76.05 34.21 4.66 40.39 118.23
130 1 -67.39 -34.19 -4.14 -76.21 28.27
21 79.50 34.19 4.14 76.21 120.72
140 1 -64.92 -34.16 -4.96 -59.92 49.32
21 77.03 34.16 4.96 59.92 129.25
100 21 -432.69 -2.89 -4.34 -21.26 11.14
35 451.52 2.89 4.34 21.26 197.28
MOM-Z
303.66
-86.56
305.35-
-89.59
305.45
-86.65
98.94
-172.73
75.47
-247.04
80.86
-180.27
80.68
-182.57
79.90
-182.22
153.85
-165.18
-63.55
-267.39
71.98
-179.90
72.55
-183.97
73.25
-180.37
-590.75
-393.14
-1375.88
-714.43
-776.62
-454.92
-777.29
-453.57
-775.37
-454.31
-99.15
-39.48
65


STAAD SPACE
*;C#*:t;:tc***********:t;*:|:**:t:#*##*##**************** *******
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE -- POUN INCH
MEM8 LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y
110 21 -784.20 -2.95 -2.96 -0.78 50.45
35 800.34 2.95 2.96 0.78 91.81
120 21 -555.39 -2.84 -3.25 -18.71 45.15
35 572.03 2.84 3.25 18.71 110.84
130 21 -761.75 -3.08 -5.94 -45.55 130.85
35 777.89 3.08 5.94 45.55 154.23
140 21 -676.68 -3.16 -4.65 -33.28 101.81
35 692.82 3.16 4.65 33.28 121.30
32 100 35 -453.85 -13.26 30.07 97.09 -173.30
43 460.13 13.26 -30.07 -97.09 -307.80
110 35 -804.32 -8.21 31.14 68.12 -105.33
43 809.70 8.21 -31.14 -68.12 -392.86
120 35 -572.70 -12.36 6.11 89.96 -64.42
43 578.08 12.36 -6.11 -89.96 -33.28
130 35 -779.55 -15.42 38.76 101.27 -130.27
43 784.93 15.42 -38.76 -101.27 -489.91
140 35 -692.62 -15.29 9.40 100.34 -61.19
43 698.00 15.29 -9.40 -100.34 -89.27
33 100 21 338.73 12.69 2.21 -9.67 -75.94
47 -313.63 14.37 -2.21 9.67 -131.99
110 21 241.27 11.01 1.32 -14.97 -1.14
47 -219.75 12.19 -1.32 14.97 -123.38
120 21 358.68 10.98 3.22 -17.37 -80.66
47 -337.17 12.22 -3.22 17.37 -222.10
130 21 647.61 10.47 7.45 -67.57 -234.21
47 -626.09 12.72 -7.45 67.57 -466.64
140 21 532.71 10.88 6.11 -40.61 -174.86
47 -511.20 12.32 -6.11 40.61 -400.54
34 100 23 347.45 13.76 -1.99 10.39 2.78
47 -322.34 13.31 1.99 -10.39 184.38
110 23 256.04 11.82 -1.29 12.90 -4.47
47 -234.52 11.38 1.29 -12.90 126.29
120 23 367.80 11.81 -2.29 23.06 14.29
47 -346.28 11.39 2.29 -23.06 201.07
130 23 645.47 12.67 -7.86 63.92 109.52
47 -623.95 10.53 7.86 -63.92 629.87
140 23 537.57 12.09 -5.29 45.09 79.40
47 -516.05 11.11 5.29 -45.09 418.87
MOM-Z
-77.41
-64.26
-90.53
-45.74
-96.08
-51.98
-100.79
-50.72
-15.33
-196.91
-57.77
-73.65
27.52
-225.22
77.64
-324.37
100.46
-345.12
161.32
-240.51
150.36
-205.65
144.52
-202.95
131.92
-237.77
143.19
-210.64
222.49
-201.39
193.66
-172.77
192.58
-172.62
224.48
-123.46
203.61
-157.23
66


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
MEMB LOAD JT AXIAL SHEAR-Y
35 100 5 -43.19 26.18
23 57.31 -26.18
110 5 -35.09 18.47
23 47.20 -18.47
120 5 -36.04 21.17
23 48.15 -21.17
130 5 -30.07 21.09
23 42.17 -21.09
140 5 -33.82 21.12
23 45.93 -21.12
36 100 23 -444.95 4.85
36 463.77 -4.85
110 23 -695.89 3.94
36 712.03 -3.94
120 23 -534.34 4.42
36 550.47 -4.42
130 23 -709.23 6.18
36 725.37 -6.18
140 23 -643.85 5.36
36 659.98 -5.36
37 100 36 -465.51 8.38
50 471.78 -8.38
110 36 -716.08 5.32
50 721.46 -5.32
120 36 -550.94 8.65
50 556.32 -8.65
130 36 -722.20 17.16
50 727.57 -17.16
140 36 -658.13 13.40
50 663.51 -13.40
38 100 6 -91.82 -32.20
24 105.95 32.20
110 6 -77.56 -47.67
24 89.66 47.67
120 6 -78.11 -33.53
24 90.21 33.53
130 6 -72.80 -31.13
24 84.90 31.13
SHEAR-Z TORSION MOM-Y MOM-Z
-2.36 7.49 -23.42 635.51
2.36 -7.49 108.30 307.14
' 1.83 31.42 -132.14 471.22
-1.83 -31.42 66.12 193.81
-1.41 22.47 -43.67 520.55
1.41 -22.47 94.35 241.69
-3.01 23.25 15.33 524.31
3.01 -23.25 93.13 234.99
-2.51 32.58 -14.65 520.84
2.51 -32.58 105.13 239.59
-4.60 -33.25 -0.79 94.80
4.60 33.25 221.48 137.85
-2.78 -24.31 13.61 71.32
2.78 24.31 119.66 117.87
-3.04 -25.22 16.33 88.68
3.04 25.22 129.39 123.42
-11.00 -38.93 139.82 126.12
11.00 38.93 388.40 170.57
-6.09 -26.15 81.63 112.24
6.09 26.15 210.66 145.04
35.45 -54.48 -190.41 -34.10
-35.45 54.48 -376.79 168.20
34.14 -27.61 -132.89 -1.61
-34.14 27.61 -413.41 86.72
9.79 -61.13 -79.70 -80.80
-9.79 61.13 -76.91 219.24
77.61 -152.21 -301.01 -184.47
-77.61 152.21 -940.80 458.96
24.13 -98.13 -128.43 -177.43
-24.13 98.13 -257.69 391.78
-12.68 -35.32 187.49 -684.45
12.68 35.32 268.89 -474.68
-2.84 -43.88 77.93 -1072.59
2.84 43.88 24.23 -643.49
-7.89 -38.57 137.97 -729.39
7.89 38.57 145.96 -477.82
-6.30 -63.36 112.66 -680.57
6.30 63.36 114.27 -439.99
67


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
MEMB LOAD JT AXIAL SHEAR-Y
140 6 -75.97 -32.37
24 88.07 32.37
39 100 24 -166.26 -7.52
37 185.09 7.52
110 24 -148.94 -11.91
37 165.08 11.91
120 24 -144.24 -6.55
37 160.38 6.55
130 24 -132.48 -3.80
37 148.62 3.80
140 24 -139.66 -4.04
37 155.80 4.04
40 100 37 -235.05 -99.56
70 241.32 99.56
110 37 -219.56 -67.38
70 224.94 67.38
120 37 -210.09 -128.52
70 215.47 128.52
130 37 -196.54 -166.96
70 201.92 166.96
140 37 -207.46 -189.97
70 212.84 189.97
41 100 10 -99.21 21.49
27 113.33 -21.49
110 10 -82.93 17.01
27 95.03 -17.01
120 10 -84.16 17.52
27 96.26 -17.52
130 10 -91.29 17.86
27 103.39 -17.86
140 10 -86.13 17.11
27 98.23 -17.11
42 100 27 -134.23 6.88
38 153.05 -6.88
110 27 -107.63 6.53
38 123.76 -6.53
120 27 -113.25 4.97
38 129.39 -4.97
SHEAR-Z TORSION MOM-Y MOM-Z
-7.05 -50.71 131.77 -703.62
7.05 50.71 122.11 -461.65
-2.12 -8.72 -21.10 -224.72
2.12 8.72 122.63 -136.34
-1.22 18.79 40.92 -296.35
1.22 -18.79 17.48 -275.48
-3.01 -4.18 33.52 -203.98
3.01 4.18 110.85 -110.19
-1.61 -38.04 38.61 -152.73
1.61 38.04 38.51 -29.46
-3.30 -19.23 56.55 -166.50
3.30 19.23 101.76 -27.29
-32.62 44.74 -5.85 -695.34
32.62 -44.74 527.80 -897.67
-34.77 51.68 38.60 -658.34
34.77 -51.68 517.78 -419.67
-9.93 63.19 0.40 -773.40
9.93 -63.19 158.46 -1282.95
-44.47 82.45 107.84 -887.54
44.47 -82.45 603.68 -1783.87
-15.14 95.99 39.35 -970.95
15.14 -95.99 202.90 -2068.60
-11.35 47.96 152.09 676.05
11.35 -47.96 256.37 97.44
-6.53 56.41 68.49 561.00
6.53 -56.41 166.66 51.50
-8.43 54.74 116.72 561.27
8.43 -54.74 186.74 69.56
-11.72 48.94 178.01 581.44
11.72 -48.94 244.05 61.40
-9.32 62.32 141.27 554.12
9.32 -62.32 194.15 61.76
-3.05 -80.22 6.66 74.66
3.05 80.22 139.87 255.37
-0.38 -50.76 -22.69 73.25
0.38 50.76 41.12 240.07
-3.23 -63.41 26.55 59.12
3.23 63.41 128.37 179.34
68


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE
MEMB LOAD JT
130 27
38
140 27
38
43 100 38
51
110 38
51
120 38
51
130 38
51
140 38
51
44 100 7
25
110 7
25
120 7
25
130 7
25
140 7
25
45 100 25
132
110 25
132
120 25
132
130 25
132
140 25
132
46 100 9
26
110 9
26
- POUN INCH
AXIAL SHEAR-Y
-126.97 5.35
143.11 -5.35
-117.81 3.96
133.95 -3.96
-211.03 98.78
217.30 -98.78
-168.75 59.99
174.13 -59.99
-180.80 126.11
186.18 -126.11
-201.81 168.28
207.19 -168.28
-190.25 189.12
195.63 -189.12
5.71 -6.04
8.41 6.04
-45.86 5.90
57.96 -5.90
-11.71 -0.96
23.81 0.96
-11.69 3.05
23.79 -3.05
-12.42 1.17
24.52 -1.17
11.68 -18.97
7.15 18.97
-13.05 -20.64
29.19 20.64
1.48 -17.90
14.66 17.90
1.47 -15.64
14.67 15.64
0.14 -17.45
15.99 17.45
23.49 6.93
-9.37 -6.93
43.82 13.05
-31.71 -13.05
SHEAR-Z TORSION
-4.31 -82.55
4.31 82.55
-4.35 -70.78
' 4.35 70.78
-37.09 -11.84
37.09 11.84
-33.12 -3.87
33.12 3.87
-11.47 -40.82
11.47 40.82
-87.21 -135.18
87.21 135.18
-29.80 -110.30
29.30 110.30
10.55 16.94
-10.55 -16.94
-10.23 33.12
10.23 -33.12
3.05 20.59
-3.05 -20.59
3.50 -3.12
-3.50 3.12
3.21 12.68
-3.21 -12.68
3.36 -19.92
-3.36 19.92
-1.10 -13.70
1.10 13.70
1.51 -17.55
-1.51 17.55
1.70 -46.73
-1.70 46.73
1.49 -28.39
-1.49 28.39
6.21 -18.39
-6.21 18.39
12.76 60.95
-12.76 -60.95
MOM-Y MOM-Z
70.84 75.54
136.26 181.41
60.76 57.04
147.83 132.96
-30.64 632.68
624.15 947.82
38.32 471.58
491.67 488.19
-15.68 671.71
199.21 1346.01
34.48 830.78
1360.83 1861.73
0.66 873.62
476.19 2147.37
-562.16 -62.98
182.34 -154.53
352.56 251.12
15.69 -38.60
-212.60 53.99
102.77 -88.52
-220.81 128.70
94.71 -18.76
-207.60 92.07
92.17 -50.00
-175.65 -401.94
14.38 -508.72
10.45 -462.73
42.18 -528.04
-93.39 -385.16
20.95 -473.85
-88.72 -331.99
6.89 -418.62
-86.02 -372.12
14.46 -465.42
-504.42 182.70
280.88 66.95
-662.74 264.84
203.52 204.99
69


STAAD SPACE
************** *************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
UNITS ARE POUN INCH
LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
120 9 26.19 8.28 7.53 9.71 -493.20 191.59
26 -14.09 -8.28 -7.53 -9.71 222.07 106.37
130 9 26.22 10.84 7.89 -14.50 -488.90 249.55
26 -14.12 -10.84 -7.89 14.50 204.76 140.55
140 9 24.82 9.25 7.57 2.85 -482.08 211.90
26 -12.71 -9.25 -7.57 -2.85 209.55 121.05
100 26 -6.79 11.99 6.55 -35.19 -290.41 143.09
131 25.62 -11.99 -6.55 35.19 -23.97 432.62
110 26 5.70 14.75 5.82 -46.43 -214.53 221.98
131 10.44 -14.75 -5.82 46.43 -64.83 486.14
120 26 -3.60 11.77 5.51 -32.50 -230.49 153.05
131 19.73 -11.77 -5.51 32.50 -33.81 412.15
130 26 -6.41 14.04 5.86 -54.74 -237.96 192.94
131 22.55 -14.04 -5.86 54.74 -43.10 480.96
140 26 -5.92 12.58 5.48 -37.42 -225.68 164.73
131 22.05 -12.58 -5.48 37.42 -37.40 439.27
100 25 -5.06 2.28 0.34 9.52 -32.78 -116.20
26 5.06 16.16 -0.34 -9.52 16.80 -210.04
110 25 -1.70 -10.21 -6.94 11.01 218.62 -424.35
26 1.70 26.01 6.94 -11.01 107.38 -426.97
120 25 -3.50 -1.88 -2.02 8.41 52.95 -200.20
26 3.50 17.68 2.02 -8.41 42.21 -259.42
130 25 -3.20 -4.73 -2.04 33.20 55.52 -260.34
26 3.20 20.54 2.04 -33.20 40.24 -333.49
140 25 -3.33 -2.84 -2.09 16.13 57.93 -218.88
26 3.33 18.64 2.09 -16.13 40.27 -285.77
100 24 7.87 40.80 -6.85 2.83 252.33 811.76
25 -7.87 -22.37 6.85 -2.83 69.65 672.68
110 24 24.84 50.52 2.20 -15.13 68.54 1077.36
25 -24.84 -34.72 -2.20 15.13 -171.79 925.67
120 24 13.44 39.22 -3.57 -0.97 182.44 798.20
25 -13.44 -23.42 3.57 0.97 H 00 1 673.89
130 24 15.49 36.34 -3.84 27.21 192.17 725.69
25 -15.49 -20.54 3.84 --27.21 -11.91 611.09
140 24 15.29 37.65 -3.81 9.98 195.69 757.03
25 -15.29 -21.84 3.81 . -9.98 -16.86 641.00
100 38 -95.44 47.17 6.00 5.05 -160.24 991.80
131 95.44 -29.91 -6.00 -5.05 -103.98 704.13
70


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE -- POUN INCH
MEMB LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y
110 38 -54.84 38.30 4.18 -23.70 -87.69
131 54.84 -23.51 -4.18 23.70 -96.21
120 38 -125.37 41.14 4.58 -4.38 -122.16
131 125.37 -26.34 -4.58 4.38 -79.41
130 38 -173.90 44.78 5.72 15.44 -185.28
131 173.90 -29.99 -5.72 -15.44 -66.55
140 38 -193.20 43.71 4.76 1.15 -145.67
131 193.20 -28.91 -4.76 -1.15 -63.90
51 100 131 -83.45 4.28 -0.54 29.03 68.79
132 83.45 14.16 0.54 -29.03 -43.19
110 131 -40.08 13.06 -1.64 41.13 49.78
132 40.08 2.74 1.64 -41.13 27.32
120 131 -113.60 6.59 -0.93 29.43 46.91
132 113.60 9.21 0.93 -29.43 -3.43
130 131 -159.87 7.43 -0.13 58.54 11.81
132 159.87 8.37 0.13 -58.54 -5.61
140 131 -180.62 6.85 -0.72 38.55 26.48
132 180.62 8.96 0.72 -38.55 7.27
52 100 37 -102.42 39.74 -3.90 14.65 160.24
132 102.42 -21.31 3.90 -14.65 23.27
110 37 -60.72 47.73 -0.54 -1.05 66.59
132 60.72 -31.93 0.54 1.05 -41.02
120 37 -131.49 39.67 -2.43 8.48 128.53
132 131.49 -23.86 2.43 -8.48 -14.12
130 37 -175.50 38.83 -1.84 51.65 127.44
132 175.50 -23.03 1.84 -51.65 -41.12
140 37 -198.07 40.74 -2.21 24.09 139.48
132 198.07 -24.94 2.21 -24.09 -35.66
53 100 15 -92.13 32.13 12.04 -27.69 -184.60
31 106.25 -32.13 -12.04 27.69 -248.71
110 15 -14.47 24.05 -22.36 -7.89 741.67
31 26.57 -24.05 22.36 7.89 63.12
120 15 231.68 9.41 -145.63 31.99 4139.64
31 -219.57 -9.41 145.63 -31.99 1103.09
130 15 -73.11 24.97 8.64 -54.27 -132.79
31 85.21 -24.97 -8.64 54.27 -178.25
140 15 234.00 8.29 -146.12 18.96 4145.06
31 -221.90 -8.29 146.12 -18.96 1115.12
MOM-Z
827.91
531.88
893.68
590.84
998.30
646.67
979.19
618.43
-271.51
39.38
-45.74
288.12
-178.70
117.27
-165.71
143.76
-179.16
129.61
886.50
548.10
1055.86
816.16
901.81
591.13
891.34
562.37
948.50
595.02
691.12
465.49
528.34
337.59
255.85
83.06
536.50
362.26
229.95
68.36
71


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
MEMB LOAD JT AXIAL SHEAR-Y
54 100 31 -167.69 10.51
40 186.51 -10.51
110 31 14.68 6.68
40 1.46 -6.68
120 31 618.84 -3.47
40 -602.71 3.47
130 31 -130.58 4.31
40 146.72 -4.31
140 31 623.82 -6.35
40 -607.68 6.35
55 100 40 -235.83 75.25
57 242.11 -75.25
110 40 19.23 51.04
57 -13.85 -51.04
120 40 864.39 -9.68
57 -859.01 9.68
130 40 -188.80 152.14
57 194.18 -152.14
140 40 867.95 65.15
57 -862.57 -65.15
56 100 11 -99.02 -21.64
28 113.14 21.64
110 11 -15.76 -15.98
28 27.86 15.98
120 11 236.55 -7.52
28 -224.45 7.52
130 11 -91.30 -18.79
28 103.40 18.79
140 11 234.76 -7.28
28 -222.66 7.28
57 100 28 -133.60 -5.92
39 152.42 5.92
110 28 42.04 -3.13
39 -25.90 3.13
120 28 616.87 2.83
39 -600.73 -2.83
130 28 -127.42 -4.17
39 143.56 4.17
SHEAR-Z TORSION MOM-Y MOM-Z
3.15 -12.77 -4.03 271.75
-3.15 12.77 -147.37 232.62
-53.56 -6.67 1069.56 168.39
53.56 6.67 1501.33 151.97
-266.69 -18.50 5126.87 -106.48
266.69 18.50 7674.12 -60.12
1.55 -49.42 -12.75 152.60
-1.55 49.42 -61.88 54.23
-267.11 -33.35 5118.29 -149.39
267.11 33.35 7702.98 -155.39
28.21 -27.15 15.18 504.14
-28.21 27.15 -466.49 699.80
-66.57 -70.91 -865.47 315.03
66.57 70.91 1930.58 501.55
-380.52 -269.06 -4218.20 -153.22
380.52 269.06 10306.54 -1.65
37.30 30.49 -89.44 708.29
-37.30 -30.49 -507.36 1725.94
-367.08 -212.12 -4269.67 78.74
367.08 212.12 10142.99 963.74
11.04 54.57 -146.15 -672.16
-11.04 -54.57 -251.37 -106.90
-25.02 60.18 791.42 -484.93
25.02 -60.18 109.33 -90.30
-151.02 88.11 4176.33 -181.54
151.02 -88.11 1260.29 -89.32
12.43 46.63 -186.56 -588.94
-12.43 -46.63 -261.08 -87.32
-149.83 96.73 4150.90 -174.68
149.83 -96.73 1243.01 -87.37
3.04 -89.31 -5.91 -58.83
-3.04 89.31 -139.83 -225.39
-53.32 -71.06 1061.77 -26.32
53.32 71.06 1497.35 -124.04
-262.00 -75.17 5048.48 43.71
262.00 75.17 7527.63 92.18
5.09 -93.42 -60.47 -53.43
-5.09 93.42 -184.02 -146.71
72


STAAD SPACE
#*##***#******#****x*********************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE
MEMB LOAD JT
140 28
39
58 100 39
64
110 39
64
120 39
64
130 39
64
140 39
64
59 100 14
30
110 14
30
120 14
30
130 14
30
140 14
30
60 100 30
134
110 30
134
120 30
134
130 30
134
140 30
134
61 100 12
29
110 12
29
120 12
29
- poun : INCH
AXIAL SHEAR-Y
612.56 4.39
-596.42 -4.39
-210.16 -62.81
216.44 62.81
42.14 -40.24
-36.76 40.24
860.01 10.23
-854.63 -10.23
-201.17 -146.47
206.55 146.47
851.67 -65.77
-846.29 65.77
6.67 6.36
7.45 -6.36
20.62 1.64
-8.52 -1.64
76.88 -15.36
-64.78 15.36
5.14 0.92
6.97 -0.92
76.06 -17.51
-63.96 17.51
13.68 19.32
5.15 -19.32
17.06 12.52
-0.92 -12.52
38.01 -5.17
-21.88 5.17
10.37 14.28
5.77 -14.28
36.40 -5.61
-20.26 5.61
22.98 -7.13
-8.86 7.13
27.99 -1.52
-15.88 1.52
60.36 13.59
-48.25 -13.59
SHEAR-Z TORSION
-261.21 -82.11
261.21 82.11
38.61 -15.59
-38.61 15.59
-60.60 44.96
60.60 -44.96
-367.17 255.21
367.17 -255.21
64.08 -150.84
-64.08 150.84
-348.49 167.86
348.49 -167.86
-10.37 13.43
10.37 -13.43
-19.12 23.53
19.12 -23.53
-57.75 50.06
57.75 -50.06
-9.41 -12.38
9.41 12.38
-57.86 40.70
57.86 -40.70
-3.35 -24.35
3.35 24.35
-8.35 -10.13
8.35 10.13
-29.27 10.77
29.27 -10.77
-3.10 -50.91
3.10 50.91
-29.32 -0.82
29.32 0.82
-6.13 -24.31
6.13 24.31
-11.21 0.50
11.21 -0.50
-33.79 61.37
33.79 -61.37
MOM-Y MOM-Z
5026.90 54.57
7511.32 156.17
38.33 -648.79
-656.11 -356.17
-860.20 -427.09
1829.83 -216.80
-4176.34 43.75
10050.98 119.96
61.64 -860.95
-1086.88 -1482.55
-4177.95 -197.33
9753.80 -854.93
559.79 68.43
-186.62 160.51
916.49 -26.59
-228.24 85.62
2567.64 -398.11
-488.80 -154.85
487.24 -25.12
-148.48 58.17
2563.43 -436.55
-480.63 -193.96
177.11 414.84
-16.43 512.42
256.20 273.97
144.82 326.79
655.81 -90.30
748.98 -157.85
147.50 298.93
1.44 386.38
650.61 -103.78
756.59 -165.48
502.41 -182.91
-281.79 -73.86
803.88 -31.67
-400.19 -22.98
2203.99 385.51
-987.65 103.76
73


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE -- POUN INCH
MEMB LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
130 12 18.72 -8.46 -5.57 -42.89 423.23 -210.10
29 -6.62 8.46 5.57 42.89 -222.72 -94.31
140 12 58.78 12.75 -33.86 53.63 2194.91 368.07
29 -46.67 -12.75 33.86 -53.63 -975.78 90.84
62 100 29 -7.25 -11.53 -6.68 -39.87 295.84 -133.10
133 26.08 11.53 6.68 39.87 25.01 -420.18
110 29 4.20 -7.61 -12.80 -47.65 405.63 -101.24
133 11.94 7.61 12.80 47.65 208.79 -263.83
120 29 41.82 -1.36 -39.43 -118.95 987.10 -96.84
133 -25.68 1.36 39.43 118.95 905.51 31.40
130 29 -10.04 -12.41 -5.91 -53.72 258.56 -158.62
133 26.18 12.41 5.91 53.72 25.08 -437.06
140 29 39.34 -2.20 -39.43 -124.58 983.91 -109.24
133 -23.20 2.20 39.43 124.58 908.69 3.66
63 100 30 8.56 -23.43 -6.46 4.54 79.46 -693.60
31 -8.56 41.86 6.46 -4.54 224.28 -840.74
110 30 4.79 -12.64 -9.18 33.40 156.40 -414.51
31 -4.79 28.44 9.18 -33.40 274.90 -550.71
120 30 -4.77 17.39 -22.84 166.45 484.84 307.03
31 4.77 -1.59 22.84 -166.45 588.50 138.94
130 30 9.40 -16.47 -5.97 34.86 65.31 -517.00
31 -9.40 32.27 5.97 -34.86 215.17 -628.42
140 30 -3.05 19.09 -22.97 178.10 481.30 342.35
31 3.05 -3.29 22.97 -178.10 598.49 183.55
64 100 29 -4.39 16.14 0.56 14.05 15.56 206.96
30 4.39 2.30 -0.56 -14.05 -41.68 118.26
110 29 -6.09 11.71 1.59 5.44 48.15 124.23
30 6.09 4.09 -1.59 -5.44 -122.74 54.92
120 29 -14.95 6.44 5.64 -0.57 180.32 -6.92
30 14.95 9.36 -5.64 0.57 -445.56 -61.88
130 29 -3.96 16.68 0.34 35.85 10.83 252.93
30 3.96 -0.88 -0.34 -35.85 -26.78 159.89
140 29 -14.95 7.34 5.57 8.11 178.20 18.40
30 14.95 8.46 -5.57 -8.11 -439.79 -44.61
65 100 40 -69.08 38.20 -3.48 17.36 130.46 824.42
134 69.08 -19.76 3.48 -17.36 32.94 537.66
110 40 -50.82 26.10 -8.52 172.08 252.41 531.48
134 50.82 -10.30 8.52 -172.08 148.06 324.05
74


STAAD SPACE
fc****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
MEMB LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y
120 40 -12.15 -0.66 -29.53 793.03 805.66
134 12.15 16.46 29.53 -793.03 582.41
130 40 -157.47 33.09 -2.52 59.61 131.13
134 157.47 -17.29 2.52 -59.61 -12.66
140 40 -94.00 0.67 -29.25 810.96 812.50
134 94.00 15.14 29.25 -810.96 562.43
66 100 133 -49.76 3.82 -0.13 33.79 63.36
134 49.76 14.61 0.13 -33.79 -57.29
110 133 -38.31 4.58 -0.17 27.26 165.98
134 38.31 11.22 0.17 -27.26 -158.18
120 133 -17.32 10.38 -0.27 44.05 584.17
134 17.32 5.42 0.27 -44.05 -571.64
130 133 -143.19 4.27 0.58 58.17 10.88
134 143.19 11.53 -0.58 -58.17 -38.24
140 133 -99.62 10.67 0.06 54.37 560.28
134 99.62 5.13 -0.06 -54.37 -563.26
67 100 16 -43.24 -26.71 2.75 13.45 25.27
32 57.36 26.71 -2.75 -13.45 -124.21
110 16 -102.96 -23.65 -17.42 47.75 980.41
32 115.07 23.65 53.60 -47.75 297.80
120 16 -345.00 -26.22 -90.59 163.33 4530.67
32 357.10 26.22 261.88 -163.33 1813.93
130 16 -31.25 -22.75 4.19 11.52 -38.54
32 43.35 22.75 -4.19 -11.52 -112.16
140 16 -342.84 -26.19 -89.88 170.05 4504.34
32 354.94 26.19 261.17 -170.05 1814.67
68 100 32 -446.07 -2.60 5.22 -39.76 -18.07
41 464.90 2.60 -5.22 39.76 -232.41
110 32 -543.52 -1.13 -27.30 -17.81 805.92
41 559.66 1.13 75.54 17.81 1662.17
120 32 -1128.52 2.56 -142.34 16.38 3854.01
41 1144.65 -2.56 370.72 -16.38 8459.50
130 32 -691.45 -4.46 9.14 -40.27 -85.20
41 707.58 4.46 -9.14 40.27 -353.62
140 32 -1290.31 1.82 -140.06 19.29 3818.43
41 1306.44 -1.82 368.45 -19.29 8385.89
69 100 41 -466.89 -7.00 -36.91 -69.16 205.58
63 473.17 7.00 36.91 69.16 385.01
MOM-Z
-175.21
-226.96
742.57
441.37
-119.07
-220.99
-278.91
25.24
-153.41
-2.74
185.81
-69.11
-225.64
54.98
185.82
-55.51
-639.44
-322.21
-557.26
-294.04
-592.70
-351.14
-548.96
-270.01
-591.98
-350.85
-51.07
-73.59
-28.52
-25.79
24.23
98.80
-94.39
-119.77
3.75
83.59
-49.33
-62.66
75


STAAD SPACE
a****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y
110 41 -617.99 -9.93 -80.89 -73.20 -786.50
63 623.37 9.93 .96.97 73.20 2209.32
120 41 -1414.19 -23.52 -304.72 -128.74 -4218.73
63 1419.57 23.52 380.85 128.74 9703.34
130 41 -705.99 -17.76 -56.33 -187.41 285.45
63 711.37 17.76 56.33 187.41 615.90
140 41 -1574.72 -29.84 -320.67 -190.86 -4160.63
63 1580.10 29.84 396.79 190.86 9900.30
100 20 -44.32 26.91 6.14 -42.02 -22.33
34 58.44 -26.91 -6.14 42.02 -198.88
110 20 -101.73 23.44 -14.08 -58.96 930.69
34 113.84 -23.44 50.26 58.96 227.27
120 20 -343.96 25.02 -87.57 -162.86 4519.15
34 356.07 -25.02 258.86 162.86 1716.68
130 20 -41.51 23.02 4.69 -71.92 3.05
34 53.62 -23.02 -4.69 71.92 -171.95
140 20 -345.05 24.93 -87.81 -178.92 4522.40
34 357.15 -24.93 259.10 178.92 1721.91
100 34 -427.31 5.03 5.62 -18.19 -57.77
42 446.13 -5.03 -5.62 18.19 -211.78
110 34 -527.44 3.47 -27.56 -9.93 801.25
42 543.57 -3.47 75.80 9.93 1679.54
120 34 -1140.63 0.19 -148.70 -20.40 3981.79
42 1156.77 -0.19 377.08 20.40 8636.88
130 34 -707.43 4.56 5.40 -55.04 -103.71
42 723.57 -4.56 -5.40 55.04 -155.50
140 34 -1313.59 0.62 -147.74 -36.81 3948.69
42 1329.73 -0.62 376.13 36.81 8624.27
100 42 -447.55 9.37 -22.91 4.74 171.14
58 453.83 -9.37 22.91 -4.74 195.49
110 42 -601.12 9.94 -71.31 8.99 -818.39
58 606.50 -9.94 87.39 -8.99 2088.06
120 42 -1428.52 18.55 -292.78 12.05 -4361.30
58 1433.90 -18.55 368.91 -12.05 9654.82
130 42 -725.30 14.19 -32.86 42.31 130.47
58 730.68 -14.19 32.86 -42.31 395.37
140 42 -1601.36 23.12 -305.41 49.46 -4347.80
58 1606.74 -23.12 381.54 -49.46 9843.38
MOM-Z
-58.90
-100.03
-105.49
-270.87
124.47
-408.65
-7.18
-470.20
588.76
380.13
520.37
323.42
582.18
318.55
503.70
325.11
580.04
317.60
136.28
105.06
96.84
69.81
19.74
-10.57
125.22
93.48
32.87
-3.13
-17.40
167.35
-5.33
164.42
48.70
248.13
-113.43
340.53
-39.28
409.19
76


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
1EM3 LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM
73 100 18 42.11 -0.65 1 sO 00 00 -17.79 407.69 -8.
33 -27.98 0.65 .9.88 17.79 -51.94 -14.
110 18 36.04 -0.73 -16.53 -11.54 624.52 -14.
33 -23.94 0.73 16.53 11.54 -29.61 -11.
120 18 35.76 -1.53 -46.73 -13.83 1657.43 -45.
33 -23.65 1.53 46.73 13.83 24.98 -9.
130 18 36.22 -0.70 -8.98 -34.84 355.89 -10.
33 -24.12 0.70 8.98 34.84 -32.70 -14.
140 18 35.88 -1.58 -46.97 -21.06 1657.21 -47.
33 -23.78 1.58 46.97 21.06 33.65 -9.
74 100 32 23.09 13.55 5.54 43.81 -247.31 157.
33 -23.09 13.52 -5.54 -43.81 -134.92 -156.
110 32 52.04 11.53 8.74 24.06 -340.39 128.
33 -52.04 11.67 -8.74 -24.06 -262.83 -133.
120 32 177.67 11.37 23.81 -5.96 -819.63 113.
33 -177.67 11.83 -23.81 5.96 -823.22 -128.
130 32 -333.42 11.59 5.28 54.56 -251.39 136.
33 333.42 11.61 -5.28 -54.56 -113.09 -137.
140 32 -4.98 11.31 24.10 -2.25 -845.03 111.
33 4.98 11.89 -24.10 2.25 -817.67 -131.
75 100 33 23.74 14.47 -4.34 -8.13 117.13 170.
34 -23.74 12.60 4.34 8.13 182.49 -106.
110 33 52.77 12.28 -7.78 -5.55 251.29 144.
34 -52.77 10.92 7.78 5.55 285.73 -98.
120 33 179.20 11.82 -22.92 19.02 809.38 138.
34 -179.20 11.38 22.92 -19.02 772.39 -122.
130 33 -332.72 12.51 -3.70 21.86 78.25 151.
34 332.72 10.69 3.70 -21.86 176.72 -88.
140 33 -3.40 11.89 -22.87 31.40 796.60 141.
34 3.40 11.31 22.87 -31.40 781.51 -121.
76 100 18 -252.99 13.45 3.21 89.28 -180.53 171.
32 267.11 13.61 -3.21 -89.28 -69.47 -178.
110 18 -245.62 11.75 6.96 91.46 -339.60 155.
32 257.73 11.45 -6.96 -91.46 -202.19 -143.
120 18 -350.24 12.49 22.53 159.36 -1059.27 182.
32 362.34 10.71 -22.53 -159.36 -694.23 -113.
130 18 -211.79 11.58 3.34 89.45 -190.49 151.
32 223.89 11.62 -3.34 -89.45 -69.39 -153.
i-2
62
75
80
36
91
30
83
41
21
62
22
07
80
35
21
97
39
15
75
69
82
18
71
00
27
89
56
66
31
33
91
13
18
22
55
49
85
39
77


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
MEMB LOAD JT AXIAL SHEAR-Y
140 18 -347.35 12.55
32 359.45 10.65
77 100 18 -242.04 14.42
34 256.16 12.65
110 18 -237.25 12.11
34 249.35 11.09
120 18 -353.87 11.18
34 365.97 12.02
130 18 -213.36 12.42
34 225.46 10.78
140 18 -355.48 11.21
34 367.58 11.99
78 100 34 329.28 13.17
61 -304.17 13.89
110 34 277.50 11.37
61 -255.98 11.83
120 34 259.26 11.61
61 -237.74 11.58
130 34 770.11 10.71
61 -748.59 12.49
140 34 509.60 11.59
61 -488.09 11.61
79 100 32 349.56 13.26
61 -324.46 13.80
110 32 292.12 11.25
61 -270.60 11.95
120 32 252.57 10.91
61 -231.06 12.29
130 32 774.62 12.47
61 -753.10 10.73
140 32 499.22 11.17
61 -477.70 12.03
80 100 21 3.71 -6.96
24 -3.71 19.52
110 21 3.82 2.00
24 -3.82 8.76
120 21 1.31 -4.04
24 -1.31 14.79
SHEAR-Z TORSION MOM-Y MOM-Z
22.98 162.99 -1072.46 185.85
-22.98 -162.99 -715.72 -111.76
-2.38 -64.02 108.30 196.26
2.38 64.02 77.18 -127.28
-6.00 -77.43 285.20 158.84
6.00 77.43 182.14 -119.14
-20.99 -151.58 979.13 123.11
20.99 151.58 654.66 -155.88
-2.66 -40.21 59.77 171.28
2.66 40.21 147.04 -107.74
-21.30 -144.73 965.62 124.90
21.30 144.73 692.42 -154.95
3.78 -5.73 -166.21 179.44
-3.78 5.73 -189.21 -213.45
14.45 -130.87 -431.85 158.88
-14.45 130.87 -928.22 -180.25
55.86 -594.70 -1546.95 175.04
-55.86 594.70 -3709.96 -173.62
5.94 -41.52 -237.74 140.37
-5.94 41.52 -321.57 -224.07
57.50 -620.46 -1586.24 176.71
-57.50 620.46 -3825.47 -177.43
-3.22 3.19 57.42 203.67
3.22 -3.19 245.28 -228.86
-13.71 129.56 354.03 167.16
13.71 -129.56 935.90 -200.41
-54.90 595.96 1476.37 145.82
54.90 -595.96 3690.26 -211.11
-6.24 35.59 73.97 215.38
6.24 -35.59 512.99 -133.41
-56.80 618.96 1487.00 156.39
56.80 -618.96 3858.43 -197.07
16.80 112.36 -258.82 -178.71
-16.80 -112.36 -278.93 -244.96
10.91 137.52 -218.02 -27.83
-10.91 -137.52 -131.21 -80.28
13.55 116.41 -216.76 -120.82
-13.55 -116.41 -216.83 -130.45
78


STAAD SPACE
************************ ****************
*************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
MEMB LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y
130 21 0.86 -0.47 11.84 132.98 -161.47
24 -0.86 11.23 -11.84 -132.98 -217.50
140 21 -0.05 -3.16 13.05 128.88 -190.38
24 0.05 13.92 -13.05 -128.88 -227.17
81 100 35 -34.41 2.33 10.38 54.81 -118.36
37 34.41 10.22 -10.38 -54.81 -213.70
110 35 -34.10 4.02 5.26 122.04 -68.90
37 34.10 6.74 -5.26 -122.04 -99.49
120 35 -9.36 0.72 9.52 18.22 -108.67
37 9.36 10.04 -9.52 -18.22 -195.90
130 35 -44.70 1.67 12.34 -25.67 -146.82
37 44.70 9.09 -12.34 25.67 -247.93
140 35 -14.05 -0.16 12.14 -49.74 -133.63
37 14.05 10.91 -12.14 49.74 -254.70
82 100 28 8.01 20.45 -15.72 165.73 143.88
32 -8.01 -7.90 15.72 -165.73 359.14
110 28 28.30 -69.90 -12.85 116.62 131.24
32 -28.30 80.66 12.85 -116.62 279.84
120 28 110.95 -392.42 -10.36 45.61 163.28
32 -110.95 403.18 10.36 -45.61 168.08
130 28 7.34 24.02 -14.62 140.76 140.05
32 -7.34 -13.26 14.62 -140.76 327.65
140 28 111.35 -389.91 -11.67 32.80 178.84
32 -111.35 400.67 11.67 -32.80 194.59
83 100 39 -42.13 10.56 -4.40 -122.92 111.46
41 42.13 1.99 4.40 122.92 29.40
110 39 -5.35 -47.57 -8.80 -84.69 226.27
41 5.35 58.33 8.80 84.69 55.39
120 39 66.00 -258.79 -26.09 -6.69 689.64
41 -66.00 269.55 26.09 6.69 145.12
130 39 -65.48 12.37 -13.30 4.70 278.44
41 65.48 -1.61 13.30 -4.70 147.14
140 39 47.78 -257.53 -31.66 76.41 802.82
41 -47.78 268.28 31.66 -76.41 210.15
84 100 23 8.30 -8.34 -14.61 172.10 339.35
27 -8.30 20.90 14.61 -172.10 128.17
110 23 6.15 -1.83 -10.49 124.75 228.40
27 -6.15 12.59 10.49 -124.75 107.17
MOM-Z
-61.51
-125.67
-104.55
-168.67
-23.98
-102.13
13.52
-57.13
-46.42
-102.78
-23.96
-94.70
-60.11
-117.01
257.29
196.40
-1171.11
-1237.85
-6308.78
-6420.80
321.55
274.92
-6269.91
-6379.33
110.29
26.83
-818.68
-875.67
-4212.75
-4240.77
155.47
68.17
-4187.69
-4225.25
-204.81
263.03
-86.86
-143.98
79


STAAD SPACE
*****************************************************
MEMEER END FORCES STRUCTURE TYPE = SPACE
MEHB
UNITS ARE poun : INCH
LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
120 23 5.21 -6.22 -12.55 128.68 283.61 -157.81
27 -5.21 16.98 12.55 -128.68 118.15 -213.29
130 23 7.40 -12.82 -12.50 136.94 268.62 -267.52
27 -7.40 23.58 12.50 -136.94 131.49 -314.89
140 23 4.96 -8.81 -13.15 118.80 287.69 -199.27
27 -4.96 19.57 13.15 -118.80 133.10 -254.91
100 36 -40.05 1.73 -3.53 -103.75 21.23 -31.07
38 40.05 10.82 3.53 103.75 91.86 -114.29
110 36 -36.92 4.05 -1.38 -116.26 3.31 13.23
38 36.92 6.71 1.38 116.26 40.80 -55.74
120 36 -12.83 0.44 -4.23 -42.62 35.91 -49.69
38 12.83 10.32 4.23 42.62 99.56 -108.31
130 36 -88.62 -3.17 -10.97 13.89 113.28 -87.40
38 88.62 13.93 10.97 -13.89 237.91 -186.18
140 36 -30.23 -1.87 -8.04 32.39 71.98 -82.23
38 30.23 12.63 8.04 -32.39 185.19 -149.65
100 31 2.42 19.56 13.06 103.51 -239.20 248.21
34 -2.42 -7.01 -13.06 -103.51 -178.59 177.01
110 31 22.00 -69.70 12.58 44.23 -276.12 -1166.07
34 -22.00 80.45 -12.58 -44.23 -126.44 -1236.31
120 31 97.88 -397.69 17.65 -115.52 -538.00 -6396.41
34 -97.88 408.45 -17.65 115.52 -26.76 -6501.87
130 31 1.12 13.08 11.25 113.56 -220.01 156.14
34 -1.12 -2.32 -11.25 -113.56 -140.02 90.20
140 31 97.68 -398.66 17.68 -102.51 -546.17 -6411.49
34 -97.68 409.42 -17.68 102.51 -19.52 -6517.76
100 40 -28.53 11.13 4.34 87.66 -116.07 114.84
42 28.53 1.42 -4.34 -87.66 -22.93 40.64
110 40 4.49 -46.78 6.47 64.48 -188.16 -807.93
42 -4.49 57.54 -6.47 -64.48 -18.91 -861.15
120 40 84.30 -261.01 18.36 38.13 -555.10 -4248.95
42 -84.30 271.77 -18.36 -38.13 -32.45 -4275.60
130 40 -38.27 9.03 9.64 -19.96 -211.05 91.72
42 38.27 1.73 -9.64 19.96 -97.34 25.03
140 40 70.71 -260.89 22.50 -42.41 -633.72 -4244.27
42 -70.71 271.65 -22.50 42.41 -86.27 -4276.49
100 43 28.17 2.29 -1.22 28.10 -24.41 39.08
109 -18.46 -2.29 1.22 -28.10 54.49 17.58
80


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
MEMB
89
90
91
LOAD JT AXIAL
110 43 23.78
109 -15.46
120 43 20.55
109 -12.23
130 43 8.19
109 0.13
140 43 11.38
109 -3.06
100 109 14.53
117 -7.46
110 109 10.79
117 -4.74
120 109 10.96
117 -4.91
130 109 4.50
117 1.55
140 109 6.85
117 -0.80
100 45 62.55
110 -52.84
110 45 54.13
110 -45.81
120 45 54.41
110 -46.09
130 45 62.58
110 -54.26
140 45 57.99
110 -49.67
100 110 30.76
118 -23.70
110 110 26.41
118 -20.36
120 110 27.00
118 -20.94
130 110 31.51
118 -25.45
140 110 29.26
118 -23.21
SHEAR-Y SHEAR-Z
2.90 -3.60
-2.90 3.60
1.74 0.44
-1.74 -0.44
4.39 0.22
-4.39 -0.22
3.26 1.30
-3.26 -1.30
2.01 3.46
-2.01 -3.46
-0.79 -0.82
0.79 0.82
4.99 4.68
-4.99 -4.68
15.57 7.72
-15.57 -7.72
13.17 7.27
-13.17 -7.27
17.50 18.25
-17.50 -18.25
8.55 10.35
-8.55 -10.35
23.34 18.45
-23.34 -18.45
38.16 32.57
-38.16 -32.57
40.04 28.26
-40.04 -28.26
14.74 11.31
-14.74 -11.31
8.05 6.39
-8.05 -6.39
18.65 12.69
-18.65 -12.69
32.82 22.13
-32.82 -22.13
32.88 20.44
-32.88 -20.44
TORSION MOM-Y
21.99 67.80
-21.99 21.18
32.50 -56.29
-32.50 45.51
40.58 -89.20
-40.58 83.78
25.29 -101.76
-25.29 69.51
-96.99 -62.46
96.99 0.10
-54.13 -25.32
54.13 40.17
-107.47 -69.86
107.47 -14.45
-205.38 -121.92
205.38 -17.06
-202.53 -104.62
202.53 -26.33
26.72 -584.41
-26.72 132.83
17.15 -330.90
-17.15 74.83
41.38 -631.63
-41.38 174.98
80.86 -1079.00
-80.86 272.92
69.83 -972.23
-69.83 272.86
41.45 -163.20
-41.45 -40.46
23.78 -93.37
-23.78 -21.64
56.42 -193.96
-56.42 -34.50
106.85 -325.78
-106.85 -72.56
95.28 -308.42
-95.28 -59.45
MOM-Z
57.88
13.86
18.32
24.79
55.01
53.60
26.49
54.31
40.86
-4.66
6.32
-20.56
73.38
16.51
184.71
95.53
163.34
73.74
298.37
134.86
150.00
61.54
393.36
184.43
652.06
292.37
671.65
319.36
104.30
160.97
59.38
85.47
128.62
207.02
232.48
358.34
227.88
364.02
81


STAAO SPACE
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE -- POUN INCH
LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
100 49 46.02 13.54 -3.41 20.06 23.90 227.05
111 -36.31 -13.54 . 3.41 -20.06 60.42 108.15
110 49 36.54 7.28 -1.78 17.29 6.97 122.05
111 -28.22 -7.28 1.78 -17.29 37.16 58.01
120 49 42.51 15.90 -2.32 29.50 -20.68 266.40
111 -34.19 -15.90 2.32 -29.50 78.07 127.03
130 49 45.88 26.12 -3.93 43.34 -73.09 465.69
111 -37.56 -26.12 3.93 -43.34 170.25 180.30
140 49 48.52 26.05 -2.56 32.28 -73.53 446.03
111 -40.20 -26.05 2.56 -32.28 136.80 198.82
100 111 20.75 16.59 -1.16 29.44 -22.09 121.61
119 -13.69 -16.59 1.16 -29.44 42.90 176.99
110 111 16.66 11.46 -0.60 18.67 -14.47 87.91
119 -10.61 -11.46 0.60 -18.67 25.21 118.46
120 111 18.94 17.34 -0.81 32.35 -34.73 124.71
119 -12.89 -17.34 0.81 -32.35 49.30 187.46
130 111 20.04 20.28 -0.99 63.24 -79.27 139.22
119 -13.99 -20.28 0.99 -63.24 97.06 225.77
140 111 21.19 23.31 -0.71 47.52 -66.14 161.95
119 -15.14 -23.31 0.71 -47.52 78.87 257.56
100 50 19.43 -2.33 1.34 57.57 -67.45 -95.49
112 -9.73 2.33 -1.34 -57.57 34.36 37.92
110 50 14.58 -1.46 -1.89 44.52 39.38 -65.04
112 -6.26 1.46 1.89 -44.52 7.39 28.85
120 50 17.26 -2.49 1.88 37.44 -83.33 -87.86
112 -8.94 2.49 -1.88 -37.44 36.86 26.15
130 50 15.32 -4.01 6.30 83.20 -283.77 -165.38
112 -7.00 4.01 -6.30 -83.20 127.76 66.09
140 50 17.11 -4.61 4.14 66.92 -177.21 -171.55
112 -8.79 4.61 -4.14 -66.92 74.70 57.56
100 112 9.73 -2.33 1.34 57.57 -34.36 -37.92
120 -2.67 2.33 -1.34 -57.57 10.29 -3.95
110 112 6.25 -1.46 -1.89 44.52 -7.39 -28.85
120 -0.19 1.46 1.89 -44.52 41.41 2.53
120 112 8.93 -2.49 1.88 37.44 -36.86 -26.15
120 -2.88 2.49 -1.88 -37.44 3.07 -18.73
130 112 7.00 -4.01 6.30 83.20 -127.76 -66.09
120 -0.95 4.01 -6.30 -83.20 14.29 -6.13
82


STAAD SPACE
I*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
MEMB LOAD JT
140 112
120
96 100 109
110
110 109
110
120 109
110
130 109
110
140 109
110
97 100 117
118
110 117
118
120 117
118
130 117
118
140 117
118
98 100 118
119
110 118
119
120 118
119
130 118
119
140 118
119
99 100 110
111
110 110
111
120 110
111
AXIAL SHEAR-Y
8.78 -4.61
-2.73 4.61
-0.28 3.94
0.28 15.28
-3.69 4.68
3.69 11.80
3.25 1.30
-3.25 15.18
11.17 -4.64
-11.17 21.11
9.90 -3.78
-9.90 20.25
31.33 4.19
-31.33 15.03
19.51 4.66
-19.51 11.81
35.99 1.79
-35.99 14.69
53.11 -3.81
-53.11 20.28
56.18 -2.73
-56.18 19.20
16.59 8.66
-16.59 13.70
11.47 8.55
-11.47 10.62
17.34 6.26
-17.34 12.91
20.28 5.17
-20.28 13.99
23.31 4.01
-23.31 15.16
-3.05 6.80
3.05 15.55
-4.19 7.61
4.19 11.56
-1.45 3.92
1.45 15.25 83
SHEAR-Z TORSION
4.14 66.92
-4.14 -66.92
-4.68 -7.96
4.68 7.96
-2.77 -4.14
2.77 4.14
-4.25 -24.35
4.25 24.35
-7.50 -38.13
7.50 38.13
-5.97 -35.10
5.97 35.10
-10.16 -2.44
10.16 2.44
-5.79 -3.57
5.79 3.57
-11.88 -14.79
11.88 14.79
-21.14 -24.50
21.14 24.50
-19.73 -19.42
19.73 19.42
1.16 -42.89
-1.16 42.89
0.60 -25.21
-0.60 25.21
0.81 -49.29
-0.81 49.29
0.99 -97.05
-0.99 97.05
0.71 -78.86
-0.71 78.86
2.25 -38.33
-2.25 38.33
1.19 -22.68
-1.19 22.68
1.51 -43.34
-1.51 43.34
MOM-Y MOM-Z
-74.70 -57.56
0.15 -25.34
125.08 -58.45
104.23 -219.52
76.12 -20.18
59.62 -154.24
139.97 -98.17
68.19 -241.84
245.97 -238.30
121.60 -392.47
227.82 -217.66
64.77 -370.98
361.02 -70.99
136.75 -194.51
207.42 -30.25
76.44 -144.85
447.46 -111.07
134.85 -205.04
809.54 -257.45
226.38 -332.62
783.71 -233.37
183.06 -303.77
-95.31 33.54
29.44 -176.99
-52.65 59.38
18.67 -118.46
-78.43 -1.98
32.35 -187.46
-119.53 -25.72
63.24 -225.77
-87.78 -60.25
47.52 -257.56
-118.96 -19.64
-9.38 -229.76
-66.25 33.32
-1.38 -145.92
-83.23 -71.20
-2.85 -251.75


STAAD SPACE
******************************************
*********
**
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE -- POUN INCH
MEMB
100
101
102
103
LOAD JT AXIAL SHEAR-Y
130 110 5.85 1.64
111 -5.85 17.52
140 110 2.75 0.16
111 -2.75 19.00
100 120 1.34 2.66
121 -1.34 9.89
110 120 -1.89 0.20
121 1.89 10.56
120 120 1.87 2.88
121 -1.87 7.88
130 120 6.31 0.95
121 -6.31 9.81
140 120 4.14 2.73
121 -4.14 8.03
100 121 -357.30 12.52
122 357.30 12.78
110 121 -636.52 10.76
122 636.52 10.93
120 121 -1031.23 10.69
122 1031.23 11.00
130 121 -666.18 10.58
122 666.18 11.11
140 121 -1110.18 10.61
122 1110.18 11.07
100 122 10.03 9.19
123 -10.03 3.36
110 122 -4.04 10.82
123 4.04 -0.07
120 122 -55.91 23.06
123 55.91 -12.30
130 122 20.52 8.11
123 -20.52 2.65
140 122 -45.73 22.84
123 45.73 -12.08
100 50 -679.66 4.87
121 696.43 7.68
110 50 -1015.15 4.30
121 1029.52 6.46
SHEAR-Z TORSION MOM-Y
2.94 -90.98 -147.59
-2.94 90.98 -19.91
1.85 -70.65 -90.22
-1.85 70.65 -15.24
-2.33 3.95 57.57
2.33 -3.95 16.86
-1.46 -2.53 44.52
1.46 2.53 2.27
-2.49 18.73 37.44
2.49 -18.73 42.34
-4.01 6.13 83.21
4.01 -6.13 45.18
-4.61 25.34 66.93
4.61 -25.34 80.46
1.98 -10.85 -224.86
-1.98 10.85 96.88
0.41 -17.71 -126.30
-0.41 17.71 99.65
4.71 32.45 -304.43
-4.71 -32.45 0.36
3.51 -21.63 -372.15
-3.51 21.63 145.68
7.55 31.04 -498.75
-7.55 -31.04 11.77
32.57 89.03 -556.78
-32.57 -89.03 -485.35
24.31 72.51 -477.91
-24.31 -72.51 -300.15
14.99 87.05 -485.36
-14.99 -87.05 5.77
61.41 191.72 -1025.88
-61.41 -191.72 -939.11
41.77 169.20 -908.28
-41.77 -169.20 -428.28
-13.44 -15.47 574.50
13.44 15.47 143.44
-8.81 -10.61 403.59
8.81 10.61 66.74
MOM-Z
-132.38
-320.02
-176.27
-360.78
-10.29
-105.37
-41.41
-124.41
-3.07
-77.02
-14.29
-127.56
-0.15
-84.66
125.86
-134.16
108.15
-113.57
104.59
-114.59
101.91
-118.89
101.83
-116.65
88.88
4.34
119.92
54.30
307.28
258.57
83.16
4.15
306.52
252.33
20.84
-96.09
26.59
-84.21
84


STAAO SPACE
a****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNIT S ARE -- POUN INCH
MEMB LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y
120 50 -678.30 4.29 -13.37 -14.17 492.31
121 692.67 6.46 13.37 14.17 221.42
130 50 -1184.15 2.21 -21.39 -41.98 924.69
121 1198.52 8.54 21.39 41.98 217.69
140 50 -832.45 3.60 -23.46 -43.34 914.15
121 846.82 7.16 23.46 43.34 338.45
104 100 54 -92.29 7.24 -17.49 -65.04 736.88
121 109.05 5.41 17.49 65.04 199.57
110 54 27.39 6.43 -12.83 -44.81 536.94
121 -13.01 4.41 12.83 44.81 149.98
120 54 1039.48 2.60 -15.06 -72.71 639.10
121 -1025.11 8.25 15.06 72.71 167.46
130 54 -86.05 7.34 -30.88 -89.52 1323.50
121 100.43 3.50 30.88 89.52 329.96
140 54 1017.31 2.50 -30.39 -105.84 1317.60
121 -1002.94 8.35 30.39 105.84 309.54
105 100 54 15.85 6.48 28.49 26.09 -1057.55
122 0.92 6.16 -28.49 -26.09 -468.18
110 54 141.03 5.81 20.43 13.56 -734.23
122 -126.66 5.04 -20.43 -13.56 -359.82
120 54 -904.70 10.14 25.16 43.68 -1051.32
122 919.07 0.70 -25.16 -43.68 -296.24
130 54 336.77 5.01 41.59 74.08 -1568.37
122 -322.40 5.83 -41.59 -74.08 -658.75
140 54 -871.36 10.36 39.48 113.05 -1643.81
122 885.73 0.48 -39.48 -113.05 -470.19
106 100 58 -631.18 5.39 8.56 38.14 -432.69
122 647.95 7.16 -8.56 -38.14 -24.58
110 58 -933.47 5.68 6.43 32.71 -325.25
122 947.84 5.08 -6.43 -32.71 -18.34
120 58 -2511.22 9.70 10.58 0.41 -499.58
122 2525.59 1.06 -10.58 -0.41 -65.43
130 58 -866.14 4.16 12.23 61.19 -685.48
122 880.51 6.60 -12.23 -61.19 32.48
140 58 -2650.55 9.34 15.14 13.38 -756.25
122 2664.93 1.42 -15.14 -13.38 -52.33
107 100 60 54.68 -26.30 -10.39 32.38 416.66
114 -44.97 26.30 10.39 -32.38 -159.39
MOM-Z
17.41
-75.33
-42.22
-126.31
-4.86
-90.30
78.76
-29.63
73.23
-19.27
-60.52
-90.81
101.72
1.27
-65.94
-90.65
55.79
-47.22
53.98
-33.33
199.64
53.17
28.25
-50.01
207.88
56.68
34.39
-81.70
71.75
-55.94
238.40
-7.60
13.48
-78.85
225.55
-14.10
-463.26
-187.65
85


STAAD SPACE
XX***X*XXXX#XXX*X****#X******************** **********
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
MEMB
108
109
110
LOAD JT AXIAL SHEAR-Y
110 60 44.88 -20.55
114 -36.56 20.55
120 60 40.14 -14.29
114 -31.82 14.29
130 60 67.07 -49.22
114 -58.75 49.22
140 60 56.06 -36.23
114 -47.74 36.23
100 114 25.20 -22.90
124 -18.14 22.90
110 114 20.75 -17.78
124 -14.70 17.78
120 114 18.89 -13.98
124 -12.84 13.98
130 114 30.87 -36.60
124 -24.81 36.60
140 114 26.13 -27.10
124 -20.08 27.10
100 62 44.25 9.92
115 -34.54 -9.92
110 62 35.42 5.35
115 -27.09 -5.35
120 62 34.92 2.00
115 -26.60 -2.00
130 62 51.68 47.42
115 -43.36 -47.42
140 62 44.53 23.24
115 -36.21 -23.24
100 115 20.55 14.31
125 -13.49 -14.31
110 115 16.48 9.54
125 -10.43 -9.54
120 115 16.65 10.24
125 -10.60 -10.24
130 115 23.74 20.90
125 -17.69 -20.90
140 115 20.91 17.65
125 -14.86 -17.65
SHEAR-Z TORSION MOM-Y
-5.36 -5.33 157.89
5.36 5.33 -25.20
' 7.50 -177.90 -655.89
-7.50 177.90 470.26
-20.80 79.76 822.68
20.80 -79.76 -307.90
-2.49 -132.28 -270.03
2.49 132.28 331.73
-8.47 40.64 150.89
8.47 -40.64 1.55
-4.23 0.66 50.10
4.23 -0.66 26.03
6.54 -157.40 -276.51
-6.54 157.40 158.73
-16.47 80.83 292.98
16.47 -80.83 3.55
-1.08 -119.96 -142.76
1.08 119.96 162.21
-6.58 -55.68 320.80
6.58 55.68 -157.98
-1.18 -2.66 21.93
1.18 2.66 7.19
8.48 163.25 -703.04
-8.48 -163.25 493.19
-18.48 -136.23 815.51
18.48 136.23 -358.21
-0.50 103.99 -336.72
0.50 -103.99 349.12
-5.37 -52.74 123.14
5.37 52.74 -26.50
-0.90 1.06 5.29
0.90 -1.06 10.91
7.28 159.66 -295.11
-7.28 -159.66 164.08
-14.36 -119.43 299.28
14.36 119.43 -40.85
0.60 111.94 -166.72
-0.60 -111.94 155.87
MOM-Z
-363.11
-145.60
-257.35
-96.37
-868.65
-349.46
-645.67
-250.95
-147.15
-265.01
-113.48
-206.53
-91.45
-160.27
-219.95
-438.94
-161.56
-326.28
162.49
82.97
83.49
48.91
32.72
16.84
853.97
319.60
412.72
162.42
100.89
156.73
68.63
103.10
80.75
103.62
80.55
295.73
99.91
217.75
86


STAAD SPACE
*****************************************************
member end forces structure TYPE = SPACE
ALL UNITS ARE POUN INCH
EMB LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM
111 100 63 35.35 0.69 -0.63 -9.92 19.40 20.
116 -25.64 -0.69 .0.63 9.92 -3.77 -3.
110 63 29.90 -1.44 9.39 24.72 -294.73 -15.
116 -21.58 1.44 -9.39 -24.72 62.40 -19.
120 63 18.02 -1.44 49.77 197.16 -1506.90 -11.
116 -9.70 1.44 -49.77 -197.16 274.98 -24.
130 63 13.56 -8.97 0.72 -38.10 9.51 -185.
116 -5.24 8.97 -0.72 38.10 -27.34 -36.
140 63 7.39 -2.97 50.02 169.67 -1489.18 -63.
116 0.93 2.97 -50.02 -169.67 251.12 -9.
112 100 116 17.26 -3.70 -1.84 56.09 38.61 -20.
126 -10.20 3.70 1.84 -56.09 -5.48 -46.
110 116 13.02 -5.63 9.11 36.77 -74.88 -39.
126 -6.97 5.63 -9.11 -36.77 -89.10 -62.
120 116 0.45 -9.68 50.97 132.39 -473.06 -54.
126 5.60 9.68 -50.97 -132.39 -444.47 -119.
130 116 5.69 17.54 -3.40 179.97 86.27 207.
126 0.36 -17.54 3.40 -179.97 -25.06 108.
140 116 -4.82 2.62 48.92 224.69 -433.52 71.
126 10.87 -2.62 -48.92 -224.69 -446.99 -23.
113 100 113 3.40 -0.55 -1.93 -8.50 102.61 -162.
114 -3.40 19.77 1.93 8.50 -8.26 -334.
110 113 2.78 0.66 -1.13 24.90 61.46 -112.
114 -2.78 15.82 1.13 -24.90 -6.00 -259.
120 113 0.31 3.51 0.96 193.75 -26.40 -43.
114 -0.31 12.96 -0.96 -193.75 -20.50 -187.
130 113 12.61 -11.40 -4.33 -14.92 213.06 -392.
114 -12.61 27.88 4.33 14.92 -1.07 -569.
140 113 9.12 -5.17 -1.41 188.97 81.54 -244.
114 -9.12 21.64 1.41 -188.97 -12.32 -412.
114 100 123 22.89 1.08 -8.47 1.55 374.34 -153.
124 -22.89 18.14 8.47 -1.55 40.64 -265.
110 123 17.77 1.78 -4.23 26.03 206.58 -109.
124 -17.77 14.69 4.23 -26.03 0.66 -206.
120 123 13.98 3.65 6.54 158.73 -163.22 -64.
124 -13.98 12.83 -6.54 -158.73 -157.40 -160.
130 123 36.60 -8.34 -16.47 3.55 726.36 -373.
124 -36.60 24.82 16.47 -3.55 80.33 -438.
i-Z
57
44
85
85
21
45
75
26
58
81
44
21
05
35
55
71
76
00
06
83
81
80
29
08
76
83
91
41
37
51
15
01
76
53
60
27
40
94
87


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
117
UNITS ARE POUN INCH
LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
140 123 27.09 -3.60 -1.08 162.20 172.89 -253.61
124 -27.09 20.07 1.08 -162.20 -119.96 -326.28
100 115 -4.39 13.99 1.21 34.84 -2.93 183.36
116 4.39 8.37 -1.21 -34.84 -66.00 -23.88
110 115 -4.19 10.61 0.28 -12.48 -3.72 117.53
116 4.19 8.55 -0.28 12.48 -12.05 -58.90
120 115 -8.24 9.91 -1.20 -198.08 3.59 97.58
116 8.24 9.26 1.20 198.08 64.76 -79.00
130 115 26.52 19.61 4.12 58.92 -16.80 400.15
116 -26.52 -0.45 -4.12 -58.92 -218.07 171.50
140 115 5.59 15.26 1.10 -182.40 -7.94 262.32
116 -5.59 3.91 -1.10 182.40 -55.01 61.25
100 125 14.31 13.49 5.37 26.50 -52.74 156.73
126 -14.31 8.87 -5.37 -26.50 -253.28 -25.24
110 125 9.54 10.42 0.90 -10.91 1.06 103.10
126 -9.54 8.74 -0.90 10.91 -52.36 -55.08
120 125 10.24 10.61 -7.28 -164.08 159.66 103.62
126 -10.24 8.56 7.28 164.08 255.27 -45.17
130 125 20.91 17.69 14.36 40.86 -119.43 295.73
126 -20.91 1.47 -14.36 -40.86 -698.90 166.53
140 125 17.65 14.87 -0.60 -155.87 111.94 217.75
126 -17.65 4.29 0.60 155.87 -77.56 83.87
100 64 859.68 7.07 11.27 65.43 -410.38 192.21
127 -842.91 -7.07 -11.27 -65.43 -71.47 110.07
110 64 865.86 4.98 12.66 27.51 -451.31 137.82
127 -851.49 -4.98 -12.66 -27.51 -89.88 74.98
120 64 2989.94 11.21 39.44 78.74 -1342.81 321.39
127 -2975.56 -11.21 -39.44 -78.74 -343.25 157.86
130 64 1430.91 2.54 20.79 163.31 -711.14 33.15
127 -1416.54 -2.54 -20.79 -163.31 -177.65 75.38
140 64 3321.03 5.64 45.17 161.22 -1528.35 140.21
127 -3306.65 -5.64 -45.17 -161.22 -402.53 101.05
100 70 464.62 -2.21 -7.77 5.40 280.86 -29.52
128 -447.85 2.21 7.77 -5.40 51.40 -65.04
110 70 789.20 2.27 -12.93 4.59 442.55 94.55
128 -774.83 -2.27 12.93 -4.59 110.11 2.39
120 70 -370.08 -7.31 1.18 4.99 -11.84 -172.92
128 384.46 7.31 -1.18 -4.99 -38.57 -139.77
88


STAAD SPACE
*****************************************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
121
122
UNITS ARE POUN INCH
LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y MOM-Z
130 70 472.35 -7.86 -9.66 -43.51 323.29 -188.78
128 -457.98 7.86 9.66 43.51 89.79 -147.24
140 70 -388.21 -11.22 1.25 -45.43 -24.19 -292.35
128 402.59 11.22 -1.25 45.43 -29.19 -187.22
100 126 7.21 1.33 -10.61 -20.97 309.37 -31.98
127 -7.21 11.23 10.61 20.97 30.13 -126.40
110 126 -8.21 -1.77 -3.91 -7.27 89.13 -78.19
127 8.21 12.53 3.91 7.27 35.90 -150.74
120 126 -58.26 -14.16 -0.56 -74.54 -122.88 -280.39
127 58.26 24.92 0.56 74.54 140.84 -344.94
130 126 17.74 -1.85 -38.45 -58.53 878.87 -65.92
127 -17.74 12.60 38.45 58.53 351.39 -165.26
140 126 -49.53 -15.17 -20.27 -107.69 302.25 -291.13
127 49.53 25.93 20.27 107.69 346.44 -366.59
100 127 -502.79 12.61 -3.06 -89.74 13.80 127.95
128 502.79 12.69 3.06 89.74 183.67 -130.61
110 127 -829.74 10.79 -0.83 -51.90 -14.53 108.52
128 829.74 10.90 0.83 51.90 68.23 -111.94
120 127 -1155.76 10.75 -2.89 -86.82 -28.62 104.28
128 1155.76 10.94 2.89 86.82 215.11 -110.36
130 127 -828.08 10.75 -5.37 -152.43 -89.15 106.84
128 828.08 10.94 5.37 152.43 435.33 -113.09
140 127 -1237.42 10.68 -3.60 -118.10 -163.13 101.37
128 1237.42 11.01 3.60 118.10 395.19 -112.16
100 117 13.62 3.27 33.34 75.65 -458.01 -2.53
128 -13.62 9.28 -33.34 -75.65 -608.78 -93.54
110 117 4.97 0.08 18.72 50.80 -261.55 -43.74
128 -4.97 10.68 -18.72 -50.80 -337.53 -125.91
120 117 16.57 3.12 40.98 94.56 -554.93 -0.34
128 -16.57 7.64 -40.98 -94.56 -756.53 -72.07
130 117 28.85 2.25 68.67 161.92 -1014.92 -7.45
128 -28.85 8.51 -68.67 -161.92 -1182.46 -92.59
140 117 27.00 3.52 69.36 159.63 -986.24 6.90
128 -27.00 7.24 -69.36 -159.63 -1233.32 -66.35
100 63 -908.12 4.96 -1.50 21.55 169.91 26.53
127 924.89 7.59 1.50 -21.55 -89.67 -96.86
110 63 -1174.06 5.43 -0.44 15.09 77.60 68.77
127 1188.43 5.33 0.44 -15.09 -54.18 -66.15
89


STAAD SPACE
#*xx*xxxxxxxxxx
**XXXXXXXXXXXX*XXXXXXXXXXXXXXXXXXXXXXX
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
MEMB
123
124
125
126
LOAD JT AXIAL SHEAR-Y
120 63 -2708.98 9.24
127 2723.35 1.52
130 63 -1543.95 3.42
127 1558.32 7.34
140 63 -2987.57 8.74
127 3001.94 2.02
100 67 -72.16 7.49
127 88.92 5.16
110 67 176.12 6.38
127 -161.75 4.46
120 67 -936.27 11.07
127 950.64 -0.22
130 67 -160.36 7.92
127 174.73 2.93
140 67 -1070.84 12.10
127 1085.22 -1.25
100 67 226.37 6.57
128 -209.60 6.08
110 67 264.68 6.22
128 -250.31 4.62
120 67 1297.83 2.19
128 -1283.46 8.66
130 67 526.44 4.70
128 -512.06 6.15
140 67 1407.29 1.29
128 -1392.92 9.55
100 43 -665.13 5.13
128 681.90 7.42
110 43 -1134.74 4.37
128 1149.11 6.39
120 43 -696.60 4.43
128 710.98 6.33
130 43 -955.76 3.79
128 970.14 6.96
140 43 -764.18 4.21
128 778.55 6.55
100 128 -21.91 39.20
129 21.91 -26.45
SHEAR-Z TORSION MOM-Y
-5.16 27.99 385.03
. 5.16 -27.99 -109.53
4.93 105.22 -5.41
-4.93 -105.22 -257.66
-5.57 73.96 444.17
5.57 -73.96 -146.90
-16.12 -1.58 711.83
16.12 1.58 151.48
-8.49 10.89 356.08
8.49 -10.89 98.61
-14.04 16.20 639.74
14.04 -16.20 112.07
-30.69 -95.83 1538.57
30.69 95.83 104.94
-27.88 -76.92 1387.34
27.88 76.92 105.84
14.57 28.34 -359.01
-14.57 -28.34 -421.01
8.76 7.34 -179.29
-8.76 -7.34 -290.04
12.65 9.73 -301.44
-12.65 -9.73 -375.97
37.77 81.67 -1289.59
-37.77 -81.67 -733.12
34.16 67.05 -1213.93
-34.16 -67.05 -615.41
2.29 49.77 -184.50
-2.29 -49.77 61.95
1.89 44.49 -158.20
-1.89 -44.49 57.35
0.62 54.14 -131.14
-0.62 -54.14 97.83
5.79 62.47 -406.05
-5.79 -62.47 96.76
4.54 55.54 -334.71
-4.54 -55.54 92.47
-25.13 43.57 709.38
25.13 -43.57 107.29
MOM-Z
231.35
-25.05
3.04
-107.63
218.01
-38.67
86.09
-23.34
70.09
-18.50
224.74
77.54
121.97
11.60
258.83
98.65
56.34
-43.38
66.36
-23.34
-74.58
-98.68
14.20
-53.08
-105.73
-115.51
27.06
-88.28
28.27
-82.25
20.73
-71.30
3.07
-87.70
11.41
-74.06
628.89
437.35
90


STAAD SPACE
*************#********x******************************
MEMBER END FORCES STRUCTURE TYPE = SPACE
ALL UNITS ARE POUN INCH
MEMB
127
128
129
LOAD JT AXIAL SHEAR-Y SHEAR-Z TORSION MOM-Y
110 128 -14.94 26.54 -16.14 37.22 455.67
129 14.94 -15.61 16.14 -37.22 68.84
120 128 -24.53 43.38 -27.34 27.09 765.32
129 24.53 -32.46 27.34 -27.09 123.36
130 128 -34.19 62.81 -41.79 75.67 1202.35
129 34.19 -51.89 41.79 -75.67 155.75
140 128 -32.11 58 ..21 -42.13 58.08 1205.91
129 32.11 -47.29 42.13 -58.08 163.30
100 122 -12.57 28.22 -26.19 57.04 764.23
130 12.57 -15.47 26.19 -57.04 86.86
110 122 -10.84 23.89 -21.33 48.31 616.47
130 10.84 -12.96 21.33 -48.31 76.72
120 122 -2.36 9.92 -21.74 116.01 664.40
130 2.36 1.00 21.74 -116.01 42.08
130 122 -23.08 48.63 -43.34 98.79 1275.57
130 23.08 -37.70 43.34 -98.79 133.05
140 122 -10.25 24.95 -39.28 163.56 1189.11
130 10.25 -14.02 39.28 -163.56 87.34
100 129 -26.45 -21.92 -25.13 107.29 43.57
85 9.68 21.92 25.13 -107.29 1030.68
110 129 -15.61 -14.95 -16.14 68.84 37.23
85 1.24 14.95 16.14 -68.84 652.71
120 129 -32.46 -24.53 -27.34 123.36 27.09
85 18.09 24.53 27.34 -123.36 1141.87
130 129 -51.87 -34.19 -41.79 155.75 75.67
85 37.50 34.19 41.79 -155.75 1710.76
140 129 -47.28 -32.12 -42.13 163.31 58.08
85 32.91 32.12 42.13 -163.31 1742.97
100 130 -15.48 12.58 26.19 86.86 -57.04
87 -1.28 -12.58 -26.19 -86.86 -1062.47
110 130 -12.97 10.85 21.33 76.72 -48.31
87 -1.40 -10.85 -21.33 -76.72 -863.50
120 130 1.00 2.37 21.74 42.08 -116.01
87 -15.37 -2.37 -21.74 -42.08 -813.28
130 130 -37.72 23.09 43.34 133.05 -98.79
87 23.34 -23.09 -43.34 -133.05 -1754.09
140 130 -14.03 10.26 39.28 87.34 -163.56
87 -0.34 -10.26 -39.28 -87.34 -1515.47
MOM-Z
400.00
284.33
726.19
506.24
1112.56
751.28
1023.17
691.18
442.29
267.77
370.77
228.01
108.92
36.01
858.08
544.82
403.26
230.05
-437.85
-499.04
-284.83
-354.11
-506.24
-542.59
-751.28
-710.53
-691.18
-681.76
267.77
269.86
228.01
235.70
36.01
65.21
544.82
442.25
230.05
208.62
91