Determine the flow angles at the hub mean and tip radii of


Question:

An axial-flow compressor stage with hub and tip radii rh = 38 cm and rt = 61 cm is designed with the following data:

N = 6000 rpm,

ΔT0s = 19.5 K,

Cx = 137 m/s,

λ= 0.92,

Rm = 0.5.

Determine the flow angles at the hub, mean, and tip radii of both inlet and outlet of the rotor. Also calculate the degrees of reaction at both hub and tip.

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Mechanical Engineering: Determine the flow angles at the hub mean and tip radii of
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