Terminal-shock and restart control of a Mach 2.5, mixed-compression inlet coupled to a turbofan engine /
by Robert J. Baumbick, Peter G. Batterton, and Carl J. Daniele.

Description

Main Author

Baumbick, Robert J.

Related Names

Daniele, Carl J.
Batterton, Peter G.
Lewis Research Center.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1974.

Subjects

Air ducts > Air ducts / Aerodynamics.
Aerodynamics, Supersonic.
Airplanes > Airplanes / Turbofan engines.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Air intakes > Airplanes / Turbojet engines / Air intakes / Automatic control.

Note

Prepared at Lewis Research Center.
Cover title.

Physical Description

17 p. : ill. ; 27 cm.

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