Compressor-blade vibration and performance in a J47-23 turbojet engine under conditions of rotating stall /
by Morgan P. Hanson, Donald F. Johnson, and Andre J. Meyer, Jr.

Description

Main Author

Hanson, Morgan P.

Related Names

Meyer, Andre J.
Johnson, Donald F.
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, 1955.

Subjects

Axial flow compressors > Axial flow compressors / Blades > Axial flow compressors / Blades / Vibration.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Blades.

Note

"June 13 1955."

Physical Description

18 p. : ill. ; 27 cm.

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