Development of flow distortions in a full-scale nacelle inlet at mach numbers 0.63 and 1.6 to 2.0 /
Thomas G. Piercy and Bruce G. Chiccine.

Description

Main Author

Piercy, Thomas G.

Related Names

Chiccine, Bruce G.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1956

Subjects

Mach number.
Aerodynamics, Supersonic.
Air ducts.
Airplanes > Airplanes / Wings.

Note

"October 22, 1955."

Physical Description

67 p. : ill. ; 27 cm.

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