NASA NTRS · 19710039164
Analysis of liquid rocket engine exhaust plumes
Abstract
Liquid rocket propellant engine exhaust plume flow field, discussing mathematical models for combustion chamber, throat region and nozzle
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Greenwood, T., Prozan, R., Ratliff, A., Seymour, D.. 1971-02-01. Analysis of liquid rocket engine exhaust plumes. https://ntrs.nasa.gov/citations/19710039164
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