Figure P3-24 shows a portion of the landing gear on a light-weight, experimental aircraft. Point A is on a cross-section of the strut that attaches the wheel assembly to the aircraft frame. Draw a free-body diagram of the assembly and find the shear load, axial load, and bending moment at A if P=2 kN and a=74 mm

Transcribed Image Text:

30° shear Rshear axial P. 30° shear Rshear axial P.