Engineering
Engineering, 27.04.2021 14:50, robrod75

Air enters the rotor of an axial compressible stage with an axial velocity of 150 m/s and a tangential component of 80 m/s. The average rotor blade speed is 250 m/s. The blade angles are 48 degrees at the rotor inlet and 28 degrees at the rotor outlet (25 pts) a) Assuming the axial velocity component remains unchanged through the rotor passage, what is the change in tangential velocity ( C ) through the rotor passage

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Air enters the rotor of an axial compressible stage with an axial velocity of 150 m/s and a tangenti...

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