Q.

In a gas turbine rotor a radial stress of 300 kg/sq cm tensile and 500 kg/sq cm tangential stress have been found at a point. The maximum shear stress at this point would be

A. 500 kg/cm2
B. 250 kg/cm2
C. 595 kg/cm2
D. 750 kg/sq-cm
E. 300 kg/cm2
Answer» B. 250 kg/cm2
959
0
Do you find this helpful?
1

View all MCQs in

Machine Design

Discussion

No comments yet

Related MCQs