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Transient and steady-state performance of a single turbojet combustor with four different fuel nozzles
Turbojet combustor performance with injection of hydrogen peroxide for thrust augmentation
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Published Year
1950-1959 (2)
Subject
Airplanes--Turbojet engines--Combustion chambers--Performance (2) *
Airplanes--Motors--Thrust (1)
Airplanes--Turbojet engines--Afterburning (1)
Airplanes--Turbojet engines--Combustion (1)
Hydrogen peroxide (1)
Jet nozzles (1)
Jet planes--Fuel (1)
Author
Donlon, Richard H. (1)
Grobman, Jack S. (1)
McCafferty, Richard J. (1)
Metzler, Allen J. (1)
