Effect of afterburner lights and inlet unstarts on a mixed-compression-inlet turbofan engine operating at Mach 2.5 /
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 ; 1975.

Subjects

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

Note

Prepared at Lewis Research Center.
Cover title.

Physical Description

19 p. : ill. ; 27 cm.

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