Analysis of a stability valve system for extending the dynamic range of a supersonic inlet /
John A. Webb, Jr., and Miles O. Dustin.

Description

Main Author

Webb, John A.

Related Names

Dustin, Miles O.
Lewis Research Center.

Language(s)

English

Published

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

Subjects

Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Air intakes > Airplanes / Turbojet engines / Air intakes / Computer simulation.
Airplanes > Airplanes / Motors > Airplanes / Motors / Valves > Airplanes / Motors / Valves / Computer simulation.

Note

Prepared at Lewis Research Center.
Cover title.

Physical Description

37 p. : ill. ; 27 cm.

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