Problem 2 TO -2 ft -2 t- -2ft- -15 ft- 40 lb 60 lb 80 Ib 80 ib The internal drag truss for the wing of a light airplane is subjected to the forces shown. Determine the force in members BC, BH, and HC, and state if the members are in tension or compression.
Problem 2 TO -2 ft -2 t- -2ft- -15 ft- 40 lb 60 lb 80 Ib 80 ib The internal drag truss for the wing of a light airplane is subjected to the forces shown. Determine the force in members BC, BH, and HC, and state if the members are in tension or compression.
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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Using Method of Sections

Transcribed Image Text:What is the force on support C?
O 4 12 KN
O 4.00 kN
O 4.84 kN
O okN
Problem 2
G.
2 ft
B
15 ft-
40 Ib
-2 ft-
-2 ft-
60 Ib
80 Ib
80 Ib
The internal drag truss for the wing of a light
airplane is subjected to the forces shown. Determine the
force in members BC, BH, and HC, and state if the
members are in tension or compression.

Transcribed Image Text:Google
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What is the force on member BH? *
O 255 Ibs (T)
O 288 Ibs (C)
O 233 lbs (C)
O 242 Ibs (T)
What is the force on member BC? *
O 130 lbs (T)
O 144 lbs (C)
O 123 lbs (C)
O 137 Ibs (T)
What is the force on member HC? *
O 180 Ibs (C)
O 188 Ibs (C)
196 lbs (T)
O 173 Ibs (T)
I PN N OM
HUAWEI
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