Full-Scale Free-Jet Investigation of a Two-Shock Side-Inlet Diffuser at Mach 2.75 and a Comparison With a Single-Shock Diffuser
Description: Memorandum presenting a full-scale free-jet investigation of a two-shock side-inlet diffuser at Mach umber 2.75 in an altitude test chamber. Data were obtained over ranges of free-stream total pressure and temperature. Results regarding diffuser mass-flow ratio, critical pressure recovery, diffuser static-pressure variation, and diffuser-outlet flow conditions are provided.
Date: April 24, 1957
Creator: McAulay, John E.
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Partner: UNT Libraries Government Documents Department