Performance of experimental channeled-wall annular turbojet combustor at conditions simulating high-altitude supersonic flight.
[Part] I,
U-shaped channel walls for secondary-air entry / /
by Eugene V. Zettle and Robert Friedman..

Description

Main Author

Zettle, Eugene V.

Related Names

Friedman, Robert, 1929-
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

Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Combustion chambers > Airplanes / Turbojet engines / Combustion chambers / Performance.

Note

"March 15, 1955."

Physical Description

20 p. : ill. ; 27 cm.

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