Performance of a Mach Number 3.0 design axisymmetric double-cone external-compression inlet in the mach number range 1.97 to 0.79 /
by Owen H. Davis and Glenn A Mitchell.

Description

Main Author: Davis, Owen H.
Related Names: Mitchell, Glenn A.
Lewis Research Center.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration, 1960.
Subjects: Supersonic wind tunnels.
Inlet flow.
Graphs (charts).
Supersonic inlets.
Performance tests.
Mach number.
Air intakes.
Aerodynamics, Supersonic.
Drag (Aerodynamics)
Jet engines > Jet engines / Air intakes.
Note: "Lewis Research Center, Cleveland, Ohio."
"N 63-16136."
"April 1960"--Cover.
Physical Description: 29 p. : ill., graphs ; 27 cm.
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Item Link	Original Source
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