Transient and steady-state performance of a single turbojet combustor with four different fuel nozzles /
by Richard J. McCafferty and Richard H. Donlon.

Description

Main Author

McCafferty, Richard J.

Related Names

Donlon, Richard H.
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

Jet nozzles.
Jet planes > Jet planes / Fuel.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Combustion.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Combustion chambers > Airplanes / Turbojet engines / Combustion chambers / Performance.

Note

"Declassified October 31, 1958."
"October 21, 1955."
Cover title.

Physical Description

47 p. : ill ; 27 cm.

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