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.
Item Type:
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Partner:
UNT Libraries Government Documents Department