Calculate the loss of available energy across the rotor

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Air enters a radial blower with zero angular momentum. It leaves with an absolute tangential velocity, Vθ, of 200 ft/s. The rotor blade speed at rotor exit is 170 ft/s. If the stagnation pressure rise across the rotor is 0.4 psi, calculate the loss of available energy across the rotor and the rotor efficiency.

Reference no: EM131365966

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