Determine the internal axial force, shear force, and moment at point E of the oleo strut AB of the aircraft landing gear.

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Determine the internal axial force, shear force, and moment at point E of the oleo strut AB of the aircraft landing gear.

[A].	AE = 9.33 kip C, VE = 8.00 kip, ME = 80.0 kip-in.
[B].	AE = 11.11 kip T, VE = 6.67 kip, ME = 66.7 kip-in.
[C].	AE = 9.33 kip T, VE = 8.00 kip, ME = 80.0 kip-in.
[D].	AE = 11.11 kip C, VE = 6.67 kip, ME = 66.7 kip-in.

Answer: Option D

Explanation:

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