Ⓒ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

Ⓒ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

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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Question

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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