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The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios

The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios

By Kenneth John Kacynski

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Publish Date

1994

Publisher

National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

-

1-1 of 1 Editions

The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios

View The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios
The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios

Language: eng

Published In: 1994

Publisher: National Aeronautics and Space Administration, National Technical Information Service, distributor