Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine /
by Reeves P. Cochran and Robert P. Dengler.

Description

Main Author

Cochran, Reeves P.

Related Names

Dengler, Robert P.
Cochran, Reeves P.
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

Air-cooled engines.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Compressors > Airplanes / Turbojet engines / Compressors / Testing.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Blades > Airplanes / Turbojet engines / Blades / Cooling > Airplanes / Turbojet engines / Blades / Cooling / Testing.

Note

"Declassified February 10, 1959."
"March 15, 1955."
Cover title.

Physical Description

41 p. : ill. ; 27 cm.

Locate a Print Version

Find in a library

Viewability