Performance evaluation of a two-stage turbine designed for a ratio of blade speed to jet speed of 0.146 /
by Milton G. Kofskey.

Description

Main Author

Kofskey, Milton G.

Related Names

Lewis Research Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, [D.C.] : National Aeronautics and Space Administration, 1960.

Subjects

Turbines > Turbines / Blades > Turbines / Blades / Testing.
Liquid propellant rocket engines > Liquid propellant rocket engines / Testing.

Note

"January 1960."
Cover title.

Physical Description

35 p. : ill. ; 26 cm.

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