Analysis of the dynamic response of a supersonic inlet to flow-field perturbations upstream of the normal shock /
Gary L. Cole and Ross G. Willoh.

Description

Main Author

Cole, Gary L.

Related Names

Willoh, Ross G.
Lewis Research Center.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1975.

Subjects

Mathematical analysis.
Aerodynamics, Supersonic.
Air ducts > Air ducts / Aerodynamics.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Air intakes.

Note

Prepared at Lewis Research Center.
Cover title.

Physical Description

36 p. : ill. ; 27 cm.

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