Figure 1 shows a truss structure consisting of two bars of 1 m in length, cross-sectional area A = 5.10-4 m² and modulus of elasticity E = 200GPa. Nodes 1 and 2 are held fixed, and a force of 10 kN is applied in the x-direction at node 3. a) Form the local and global stiffness matrices, apply the boundary conditions and find the displace- ments of the nodes for the given force. Use the following formula relating the local displacements of a single bar to the local forces applied to its nodes. fix 8-+ = fjx L fjy C2 CS S² -CS -CS -S² fiy AE CS -C² Horo C gog(A) and S Ui Vi 18 CS Uj S² Vj -C² -CS -CS -S² C2 CS cin(A) whore A is the angle of orientation of the bor (1)

Mechanics of Materials (MindTap Course List)
9th Edition
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
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Chapter2: Axially Loaded Members
Section: Chapter Questions
Problem 2.8.8P
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Question 1
Bar 1
1 m
1
90°
fix
fiy
fjx
fjy
Here C = cos(0) and S
Bar 2
=
10 kN
1m
45°
Figure 1: Truss assembly formed of two bars
=
Figure 1 shows a truss structure consisting of two bars of 1 m in length, cross-sectional area A
5.10-4 m² and modulus of elasticity E 200GPa. Nodes 1 and 2 are held fixed, and a force of
10 kN is applied in the x-direction at node 3.
AE CS
L
2
a) Form the local and global stiffness matrices, apply the boundary conditions and find the displace-
ments of the nodes for the given force. Use the following formula relating the local displacements
of a single bar to the local forces applied to its nodes.
y
C² CS
S²
-C² -CS
-CS -S² CS
-C²
-CS
Ui
C²
-CS -S² Vi
CS
S²
{}
U j
Vj
sin(0), where is the angle of orientation of the bar.
(1)
Transcribed Image Text:Question 1 Bar 1 1 m 1 90° fix fiy fjx fjy Here C = cos(0) and S Bar 2 = 10 kN 1m 45° Figure 1: Truss assembly formed of two bars = Figure 1 shows a truss structure consisting of two bars of 1 m in length, cross-sectional area A 5.10-4 m² and modulus of elasticity E 200GPa. Nodes 1 and 2 are held fixed, and a force of 10 kN is applied in the x-direction at node 3. AE CS L 2 a) Form the local and global stiffness matrices, apply the boundary conditions and find the displace- ments of the nodes for the given force. Use the following formula relating the local displacements of a single bar to the local forces applied to its nodes. y C² CS S² -C² -CS -CS -S² CS -C² -CS Ui C² -CS -S² Vi CS S² {} U j Vj sin(0), where is the angle of orientation of the bar. (1)
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