* Required For nos. 38-40, satisfy the conditions of the given problem below: The internal drag truss of the wing of a light airplane is subjected to the forces shown in Determine the force in each member, and state if the members are in tension or compression. figure 3. 38. Load on member BC* 1 point H 0.61 m

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
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* Required
For nos. 38-40, satisfy the conditions
of the given problem below: The internal
drag truss of the wing of a light airplane
is subjected to the forces shown in
Determine the force in
figure 3.
each member, and state if the members
are in tension or compression.
38. Load on member BC *
1 point
H
0.61 m
0.61 m-
0.61 m
356 N
O A. 579.23 N (T)
B. 579.32 (C)
O C. 580.20 N(T)
D. 580.20 N (C)
356 N
0.61 m
-0.46 m-
267 N
178 N
Transcribed Image Text:* Required For nos. 38-40, satisfy the conditions of the given problem below: The internal drag truss of the wing of a light airplane is subjected to the forces shown in Determine the force in figure 3. each member, and state if the members are in tension or compression. 38. Load on member BC * 1 point H 0.61 m 0.61 m- 0.61 m 356 N O A. 579.23 N (T) B. 579.32 (C) O C. 580.20 N(T) D. 580.20 N (C) 356 N 0.61 m -0.46 m- 267 N 178 N
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