The internal drag truss for the wing of a light airplane is subjected to the forces shown. Determine the stress in members EF, GF and CG. The crossectional area of the truss member is a semi circle with a radius of 1.5 in. 2 ft 2 ft 2ft 50 kips 40 kips 80 kips 80 kips

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Draw the free body diagram and label properly.

The internal drag truss for the wing of a light airplane is
subjected to the forces shown. Determine the stress in members
EF, GF and CG. The crossectional area of the truss member is a
semi circle with a radius of 1.5 in.
2 ft
AD
2 ft
-2 ft
2 ft
+ 1.5 ft-
50 kips
40 kips
80 kips
80 kips
Transcribed Image Text:The internal drag truss for the wing of a light airplane is subjected to the forces shown. Determine the stress in members EF, GF and CG. The crossectional area of the truss member is a semi circle with a radius of 1.5 in. 2 ft AD 2 ft -2 ft 2 ft + 1.5 ft- 50 kips 40 kips 80 kips 80 kips
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