Investigation of a high-performance axial-flow compressor transonic inlet rotor designed for 37.5 pounds per second per square foot of frontal area: detailed blade-element performance
Description: Report presenting detailed blade-element-performance plots for a high-flow transonic inlet rotor. Information provided includes the effects of Mach number, blade loading, and angle of attack on element performance is provided.
Date: April 12, 1957
Creator: Felix, A. Richard & Savage, Melvyn
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Partner: UNT Libraries Government Documents Department