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Some studies of axisymmetric free jets exhausting from sonic and supersonic nozzles into still air and into supersonic streams (open access)

Some studies of axisymmetric free jets exhausting from sonic and supersonic nozzles into still air and into supersonic streams

Report presenting some experimental and theoretical studies of axisymmetric free jets exhausting from sonic and supersonic nozzles into still air and into supersonic streams as a way to investigate problems associated with propulsive jets. A variety of variables for each case are considered, including jet Mach number, nozzle divergence angle, jet static-pressure ratio, free-stream Mach number, and specific heat ratios.
Date: May 10, 1955
Creator: Love, Eugene S. & Grigsby, Carl E.
System: The UNT Digital Library