Calculate all nodal member forces for the truss. Use A = 0.0015 and E = 200GPa Node I is pinned, node 3 is a roller 3m 4m- displacements and all 12 kN 2 5 Fig 2. Truss for Q2 -4 m- 21 5
Calculate all nodal member forces for the truss. Use A = 0.0015 and E = 200GPa Node I is pinned, node 3 is a roller 3m 4m- displacements and all 12 kN 2 5 Fig 2. Truss for Q2 -4 m- 21 5
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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![Calculate all nodal displacements and all
member forces for the truss.
Use A = 0.0015 and E = 200GPa
Node I is pinned, node 3 is a roller
3m
4 m.
12 kN
G
Fig 2. Truss for Q2
4 m
ⒸD]
?](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F8bde5532-e6c7-4941-8c7c-137a782f7405%2Fef191024-72dd-4f67-9040-92174b2d081e%2Fyluiyro_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Calculate all nodal displacements and all
member forces for the truss.
Use A = 0.0015 and E = 200GPa
Node I is pinned, node 3 is a roller
3m
4 m.
12 kN
G
Fig 2. Truss for Q2
4 m
ⒸD]
?
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Step 1: Given
VIEWStep 2: Formulation of global element stiffness matrix
VIEWSolution
VIEWStep 3: Formulation of global element stiffness matrix for member 1, 2 and 5
VIEWStep 4: Formulation of global element stiffness matrix for member 3 and 4
VIEWStep 5: Assembling global stiffness matrix
VIEWStep 6: Relation between stiffness, displacement and force matrices
VIEWStep 7: Boundary conditions
VIEWStep 8: Determination of unknown displacement
VIEWStep 9: Support reactions
VIEWStep 10: Member forces
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