Effect of damper on overall and blade-element performance of a compressor rotor having a tip speed of 1151 feet per second and an aspect ratio of 3.6 /
by George W. Lewis and Roy D. Hager.

Description

Main Author

Lewis, George W., Jr.

Related Names

Hager, Roy D.
Lewis Research Center.

Language(s)

English

Published

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

Subjects

Damping (Mechanics)
Compressors > Compressors / Aerodynamics.
Compressors > Compressors / Blades.
Axial flow compressors.

Note

Prepared at Lewis Research Center.
Cover title.

Physical Description

88 p. : ill. ; 27 cm.

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