Characteristics of four nose inlets as measured at Mach numbers between 1.4 and 2.0

George B. Brajnikoff, Arthur W. Rogers
naca-rm-a51c12
Jun 1951


The pressure recovery, mass flow, and axial force of four bodies with nose inlets were measured at Mach numbers between 1.4 and 2.0 and angles of attack of 0, 3, 6, and 9 degrees. The Reynolds number based on the model inlet diameters varied between 0.4 and 0.8 million.

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