The planar truss with its support conditions and loads is shown in the Figure below. The cross-sectional area of the bars is A= 1 in?; The Young's modulus is E= 30 x10° psi; and the length of the bars are L1=6ft, L2=5ft, L3=3ft and L4=6 ft. a=30°, B=35°, y=55°, 0=50° Nodes 1, 2, and 3 are pinned. Determine (Write values not parameters in each case) 1. Angle defining the orientation of the element w.r.t. the Global Coordinate System X-Y 20% 2. Element stiffness matrix of each element 3. Global stiffness matrix after applying boundary conditions 4. Loading vector after applying boundary conditions 5. Displacements at nodes 4 and 5 6. Stresses

Structural Analysis
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Author:KASSIMALI, Aslam.
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Chapter2: Loads On Structures
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The planar truss with its support conditions and loads is shown in the Figure below. The cross-sectional area of the bars is
A= 1 in?; The Young's modulus is E= 30 x106 psi; and the length of the bars are L1=6ft, L2=5ft, L3=3ft and L4=6 ft.
a=30°, B=35°, y=55°, 0=50°
Nodes 1, 2, and 3 are pinned.
Determine (Write values not parameters in each case)
1. Angle defining the orientation of the element w.r.t. the Global Coordinate System X-Y 20%
2. Element stiffness matrix of each element
3. Global stiffness matrix after applying boundary conditions
4. Loading vector after applying boundary conditions
5. Displacements at nodes 4 and 5
6. Stresses
1
2
500 lbs
α
B
300 lbs
5
(3
4
X
4
3
Transcribed Image Text:The planar truss with its support conditions and loads is shown in the Figure below. The cross-sectional area of the bars is A= 1 in?; The Young's modulus is E= 30 x106 psi; and the length of the bars are L1=6ft, L2=5ft, L3=3ft and L4=6 ft. a=30°, B=35°, y=55°, 0=50° Nodes 1, 2, and 3 are pinned. Determine (Write values not parameters in each case) 1. Angle defining the orientation of the element w.r.t. the Global Coordinate System X-Y 20% 2. Element stiffness matrix of each element 3. Global stiffness matrix after applying boundary conditions 4. Loading vector after applying boundary conditions 5. Displacements at nodes 4 and 5 6. Stresses 1 2 500 lbs α B 300 lbs 5 (3 4 X 4 3
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