Effect of annular inlet baffles on rotating stall, blade vibration, and performance of an axial-flow compressor in a turbojet engine /
By Donald F. Johnson, Andre J. Meyer, Jr., and Morgan P. Hanson.

Description

Main Author

Johnson,Donald F.

Related Names

Hanson, Morgan P.
Meyer, Andre J.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1955.

Subjects

Axial flow compressors.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Compressors.

Note

"Declassified September 10, 1959."
"October 4, 1955."

Physical Description

18 p. : ill. ; 27 cm.

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