Page 82 - Aircraft Stuctures for Engineering Student
P. 82
Problems 67
Fig. P.3.5
P.3.5 Determine the maximum shear stress and the rate of twist in terms of the
applied torque T for the section comprising narrow rectangular strips shown in
Fig. P.3.5.
A~s. T~,,, = 3T/(2a + b)t2, dO/dz = 3T/G(2a + b)t3
