(ii) The two-cell wing section is shown in Figure Q4 is subjected to a counter-clockwise Torque of 25 kN.m. Determine th

[answerhappygod]

Ii The Two Cell Wing Section Is Shown In Figure Q4 Is Subjected To A Counter Clockwise Torque Of 25 Kn M Determine Th 1 (30.52 KiB) Viewed 11 times

(ii) The two-cell wing section is shown in Figure Q4 is subjected to a counter-clockwise Torque of 25 kN.m. Determine the (0) Shear stress distribution in the walls and (15 points) The rate of change of the angle of twist (5 points) (iii) Shear stress in wall 41° (5 points) The areas of cell A, E250,000 mm and cell A, = 300,000 mm². Assume Shear Modulus G-27500 N/mm2 and thickness t2 mm for all walls. T=25 kN. m where, 123 = 1,1 = 500mm, 2 112 1 112134-600mm, and 141° = 1500 mm t=2mm 1 143 II 123 141° 3 4 134 Figure Q4