Performance of a 1.15-pressure-ratio axial-flow fan stage with a blade tip solidity of 0.5 /
by Walter M. Osborn and Ronald J. Steinke.

Description

Main Author

Osborn, Walter Martin, 1918-

Related Names

Steinke, Ronald J.
Lewis Research Center.

Language(s)

English

Published

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

Subjects

Airplanes > Airplanes / Turbofan engines.
Axial flow compressors > Axial flow compressors / Testing > Axial flow compressors / Testing / Statistics.

Note

Prepared at Lewis Research Center.
Cover title.

Physical Description

94 p. : ill. ; 27 cm.

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