111. For the truss shown in Fig. P-111, calculate the stresses in members CE area of each member is 1.8 in.2. Indicate tensi DF. The cross-sectional compression (C). ce = 9260 psi (T); ode = 22.2 ksi (T); df = 18 A 8 ft B Ans. 6 ft 8 ft D 6 ft 8 ft E 30 kips F #

Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter4: Plane And Space Trusses
Section: Chapter Questions
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answer the following problems using method of joints and method of section separately in solving for the unknown forces and indicate if the forces/stresses are in tension or compression. Provide each solutions with a proper discussion and illustration.

111. For the truss shown in Fig. P-111, calculate the stresses in members CE, DE, and
DF. The cross-sectional area of each member is 1.8 in.2. Indicate tension (T) or
compression (C).
OCE = 9260 psi (T); DE = 22.2 ksi (T); DF = 18.5 ksi (C)
8 ft
Figure P-111
B
Ans.
6 ft
C
8 ft
D
6 ft
8 ft
E
30 kips
Transcribed Image Text:111. For the truss shown in Fig. P-111, calculate the stresses in members CE, DE, and DF. The cross-sectional area of each member is 1.8 in.2. Indicate tension (T) or compression (C). OCE = 9260 psi (T); DE = 22.2 ksi (T); DF = 18.5 ksi (C) 8 ft Figure P-111 B Ans. 6 ft C 8 ft D 6 ft 8 ft E 30 kips
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