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

AE = 9.33 kip C, VE = 8.00 kip, ME = 80.0 kip-in.

AE = 11.11 kip T, VE = 6.67 kip, ME = 66.7 kip-in.

AE = 9.33 kip T, VE = 8.00 kip, ME = 80.0 kip-in.

AE = 11.11 kip C, VE = 6.67 kip, ME = 66.7 kip-in.

Determine the internal axial force, shear force, and moment at point E

1.	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» E.