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Given that$$\alpha_1$$ = nozzle anglen = number of rows of moving blades, in a velocity compounded impulse turbine, the optimum blade speedratio is
$$2 \cos \alpha_1 n$$
$$\frac{n \cos \alpha_1}{2}$$
$$\frac{\cos \alpha_1}{2(n + 1)}$$
$$\frac{\cos \alpha_1}{2n}$$
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