ⒸL'avionnaire 30 in 0 1 KIP T. 2 ·20 in--20in- 1 KIP ↑ O D G 1KIP For the wing truss shown in the figure, calculate the normal stresses in member 2, 11, 6, 3, 13 7. The cross sectiona area of each member is 200 sq.in. Use method of sections only. 4 SKIP -20 in-1-20 in- 7

Mechanics of Materials (MindTap Course List)
9th Edition
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Barry J. Goodno, James M. Gere
Chapter8: Applications Of Plane Stress (pressure Vessels, Beams, And Combined Loadings)
Section: Chapter Questions
Problem 8.5.20P: A gondola on a ski lift is supported by two bent arms, as shown in the figure. Each arm is offset by...
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L'avionnaire
30 in
+
3
M
- 20 in
1 KIP
2
D
-20in
1 KIP
ED
For the wing truss shown in the figure, calculate the normal stresses
in member 2, 11, 6, 3, 13 7. The cross sectiona area of each
member is 200 sq.in. Use method of sections only.
1KIP
50
✪
.SKIP
in-
7
Ploin
Transcribed Image Text:L'avionnaire 30 in + 3 M - 20 in 1 KIP 2 D -20in 1 KIP ED For the wing truss shown in the figure, calculate the normal stresses in member 2, 11, 6, 3, 13 7. The cross sectiona area of each member is 200 sq.in. Use method of sections only. 1KIP 50 ✪ .SKIP in- 7 Ploin
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