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A technique applicable to the aerodynamic design of inducer-type multistage axial-flow compressors

Description: Report presenting a method for presenting the preliminary design calculation of high-pressure ratio, multistage, axial-flow compressors using the solid-body inducer-type design. Calculations are presented for various inlet hub-tip ratios, weight flows, and average pressure ratios per stage.
Date: March 1952
Creator: Savage, Melvyn & Beatty, Loren A.
Partner: UNT Libraries Government Documents Department