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 (Solved)
1. 500 kg/cm2
2. 250 kg/cm2
3. 595 kg/cm2
4. 750 kg/sq-cm
5. 300 kg/cm2
- b. 250 kg/cm2