Simulated altitude performance of two annular combustors with continuous axial openings for admission of primary air /
by Eugene V. Zettle and Herman Mark.

Description

Main Author

Zettle, Eugene V.

Related Names

Mark, Herman, author.
Lewis Flight Propulsion Laboratory.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, [1950]

Subjects

Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Testing.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Combustion chambers > Airplanes / Turbojet engines / Combustion chambers / Performance.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Combustion chambers > Airplanes / Turbojet engines / Combustion chambers / Aerodynamics.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Combustion chambers.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Combustion.
Airplanes > Airplanes / Turbojet engines.
Combution > Combution / Altitude, Influence of.
Aeronautics > Aeronautics / Research.

Note

On front cover: "August 3, 1950."

Physical Description

39 p. : ill. ; 27 cm.

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