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Turbojet combustor performance with injection of hydrogen peroxide for thrust augmentation

Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas

Published Year

• 1950-1959 (2)

Subject

• Air flow (1)
• Airplanes--Motors--Thrust (1)
• Airplanes--Turbojet engines (1)
• Airplanes--Turbojet engines--Afterburning (1)
• Airplanes--Turbojet engines--Combustion chambers--Performance (1)
• Charts, diagrams, etc (1)
• Combustion chambers (1)
• Hydrogen peroxide (1)
• Mathematics (1)

Author

• Grobman, Jack S. (2) *
• Graves, Charles C. (1)
• Metzler, Allen J. (1)

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