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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

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)

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