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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].	750 kg/sq-cm	[B].	500 kg/cm2
[C].	300 kg/cm2	[D].	250 kg/cm2
[E].	595 kg/cm2

Answer: Option D

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