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Question 17 (5 points) A centrifugal compressor has an equal rise across the rotor and diffuser. For an impeller tip Mach number of M2

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Question 17 (5 points) A centrifugal compressor has an equal rise across the rotor and diffuser. For an impeller tip Mach number of M2 = 1.33 (assume M2 = MT and y = 1.4), estimate the diffuser static pressure rise coefficient in the radial diffuser. = Cp 1.25 Cp=1.67 Cp=1.75 Cp=0.25

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