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

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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First published: 1994 1 language
Subjects
Heat transfer Thermal diffusion Nozzle flow Sweat cooling Film cooling Hydrogen oxygen engines Flow distribution

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