T. F. Greenwood, R. J. Prozan, A. W. Ratliff, Dave Seymour
Abstract
Liquid rocket propellant engine exhaust plume flow field, discussing mathematical models for combustion chamber, throat region and nozzle
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Liquid rocket propellant engine exhaust plume flow field, discussing mathematical models for combustion chamber, throat region and nozzle
Key concepts: Liquid-propellant rocket, Propellant, Rocket engine nozzle, Rocket engine, Aerospace engineering, Nozzle, Combustion chamber, Rocket (weapon)