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In a simple impulse turbine the nozzle angle at the entrance is 300. For maximum diagram efficiency. The blade – stepped ratio is (note : sin 300= 0.5, cos 300= 0.866 sin 150= 0.259, cos 150=0.966)  

(a)0.259                       (b)0.75

(c) 0.5                          (d)0.433

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