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Answer of q1

The document describes a structural analysis of a two member frame. It provides input data on member properties, boundary conditions, and applied loads. The output includes displacements, member forces, and diagrams of reactions, shear, moments, and axial forces under a single load case.

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Afaq Ahmed
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85 views9 pages

Answer of q1

The document describes a structural analysis of a two member frame. It provides input data on member properties, boundary conditions, and applied loads. The output includes displacements, member forces, and diagrams of reactions, shear, moments, and axial forces under a single load case.

Uploaded by

Afaq Ahmed
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
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LinPro 2.

7
File: D:\9-HERIOT WATT\9-HW LABS & UG THEIS\3-HW labs\1-mid 2022.aln
Units: kN-m

____________________________________________________________________________
Input Data

Coordinates of joints/supports
Joint X Y Rx Ry Rt
0: 1.00 1.00 1 1 0
1: 1.00 5.00 0 0 0
2: 4.00 5.00 1 1 1

Members
Member Joint I Joint J Type Releases
0: 0 1 TYPE1 111111
1: 1 2 TYPE1 111111

Cross Sections
0: TYPE1
A= 1.000E-02
I= 1.000E-04
E= 200000000.00
alpha= 1.2E-05

Load
0: Point Load
Load Case: CASE1
Load Name: Point
Coordinate System: Global
a= 0.00 Absolute from Joint I
Force X= 0.00
Force Y= 0.00
Moment M= 20.00

1: Point Load
Load Case: CASE1
Load Name: Point
Coordinate System: Global
a= 0.00 Absolute from Joint I
Force X= 0.00
Force Y= 0.00
Moment M= -20.00

Load Applied on Joints


Joint Applied Loads
1: 1

Load Applied on Members


Member Applied Loads

Load Cases
0: CASE1

Load Combinations

Masses

Masses Applied on Joints


Joint Applied Masses

============================================================================
Static Analysis Results
____________________________________________________________________________

____________________________________________________________________________
Load Case: CASE1

Displacements of joints in global CS


Joint X Y phi
0 0.000000 0.000000 0.000241
1 0.000003 0.000013 -0.000484
2 0.000000 0.000000 0.000000

Reactions in global CS
Joint Rx Ry M

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0 1.813595 -6.344612 0.000000
2 -1.813595 6.344612 -6.288216

Displacements (global CS) and forces (local CS) on members ends


Memb: 0
Joint X Y phi
0 0.000000 0.000000 0.000241
1 0.000003 0.000013 -0.000484
Axial Shear Moment
0 6.344612 1.813595 0.000000
1 6.344612 1.813595 -7.254379
Memb: 1
Joint X Y phi
1 0.000003 0.000013 -0.000484
2 0.000000 0.000000 0.000000
Axial Shear Moment
1 -1.813595 6.344612 12.745621
2 -1.813595 6.344612 -6.288216

Displacements and forces along members in local CS


Memb: 0
d(x) X Y phi
0.000 0.000000 0.000000 0.000241
0.400 0.000001 0.000095 0.000234
0.800 0.000003 0.000185 0.000212
1.200 0.000004 0.000263 0.000176
1.600 0.000005 0.000324 0.000125
2.000 0.000006 0.000361 0.000060
2.400 0.000008 0.000370 -0.000020
2.800 0.000009 0.000343 -0.000114
3.200 0.000010 0.000276 -0.000223
3.600 0.000011 0.000163 -0.000346
4.000 0.000013 -0.000003 -0.000484
d(x) Axial Shear Moment
0.000 6.344612 1.813595 0.000000
0.400 6.344612 1.813595 -0.725438
0.800 6.344612 1.813595 -1.450876
1.200 6.344612 1.813595 -2.176314
1.600 6.344612 1.813595 -2.901752
2.000 6.344612 1.813595 -3.627190
2.400 6.344612 1.813595 -4.352628
2.800 6.344612 1.813595 -5.078066
3.200 6.344612 1.813595 -5.803503
3.600 6.344612 1.813595 -6.528941
4.000 6.344612 1.813595 -7.254379
Memb: 1
d(x) X Y phi
0.000 0.000003 0.000013 -0.000484
0.300 0.000002 -0.000105 -0.000307
0.600 0.000002 -0.000175 -0.000159
0.900 0.000002 -0.000204 -0.000039
1.200 0.000002 -0.000201 0.000052
1.500 0.000001 -0.000175 0.000115
1.800 0.000001 -0.000135 0.000149
2.100 0.000001 -0.000089 0.000154
2.400 0.000001 -0.000045 0.000132
2.700 0.000000 -0.000013 0.000080
3.000 0.000000 0.000000 0.000000
d(x) Axial Shear Moment
0.000 -1.813595 6.344612 12.745621
0.300 -1.813595 6.344612 10.842237
0.600 -1.813595 6.344612 8.938853
0.900 -1.813595 6.344612 7.035470
1.200 -1.813595 6.344612 5.132086
1.500 -1.813595 6.344612 3.228703
1.800 -1.813595 6.344612 1.325319
2.100 -1.813595 6.344612 -0.578065
2.400 -1.813595 6.344612 -2.481448
2.700 -1.813595 6.344612 -4.384832
3.000 -1.813595 6.344612 -6.288216

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Structure, Load Case: CASE1

-20.00 1 2
1
0

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Structure, Masses

1 1 2
0

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Moment Diagram, Case: CASE1

-6.29

-7.25

12.75

0.00

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Shear Force Diagram, Case: CASE1

6.34 6.34

1.81

1.81

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Axial Force Diagram, Case: CASE1

-1.81 -1.81
6.34

6.34

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Reactions, Case: CASE1

1 -6.29 2
-1.81

6.34
-6.34

0
1.81

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Deformed shape, Case: CASE1

1 2

-0.000204

0.000370

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