Simulated afterburner performance with hydrogen peroxide injection for thrust augmentation /
by Allen J. Metzler and Jack S. Grobman.

Description

Main Author

Metzler, Allen J.

Related Names

Grobman, Jack S.
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, 1956.

Subjects

Hydrogen peroxide.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Afterburning.
Airplanes > Airplanes / Motors > Airplanes / Motors / Thrust.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Combustion chambers > Airplanes / Turbojet engines / Combustion chambers / Performance.

Note

"October 22, 1956."

Physical Description

xx p. : ill. ; 27 cm.

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