Aerospace Engineering > GATE 2018 > Jet Engines
An axial compressor rotor with 50% degree of reaction, operates with an axial velocity of 200 m/s. The absolute flow angle at the inlet of the rotor is 22° with reference to the axial direction. If the axial velocity is assumed to remain constant through the rotor, the magnitude of the relative velocity (in m/s) at the rotor exit is ________ (accurate to one decimal place).
Correct : 215.0 to 216.5
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