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Axial and circumferential variations of hot- gas-side heat-transfer rates in a hydrogen- oxygen rocketAxial and circumferential variations of hot gas side heat transfer coefficients in hydrogen oxygen engines for use in nozzle and injector design
Document ID
19710021262
Document Type
Other - NASA Technical Note (TN)
Authors
Quentmeyer, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Schacht, R. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1971
Subject Category
Thermodynamics And Combustion
Report/Patent Number
E-5762
NASA-TN-D-6396
Funding Number(s)
CONTRACT_GRANT: 122-29
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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