Cold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine.
I,
Design and performance of a solid blade configuration /
Jeffrey E. Haas, Milton G. Kofskey.

Description

Main Author

Haas, Jeffrey E.

Related Names

Kofskey, Milton G.
U.S. Army Air Mobility Research and Development Laboratory.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; 1975.

Subjects

Turbines > Turbines / Cooling.
Gas-turbines.
Axial flow.
Turbines > Turbines / Testing > Turbines / Testing / Performance.

Note

Prepared by Lewis Research Center and U.S. Army Air Mobility R&D Laboratory, Cleveland, Ohio, 44135.

Physical Description

21 p. : ill. ; 27 cm.

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