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Air film cooling in a nonadiabatic wall conical nozzle.Experimental data for an air-film cooled conical nozzle operating with a heated-air main stream and a water-cooled wall confirm the validity of Lieu's (1964) method for correlating film cooling data in the accelerated flow of a nonadiabatic-wall nozzle. The film cooling effectiveness modified for nonadiabatic walls by Lieu can be used to correlate film cooling under the condition that the main-stream to coolant velocity ratio at the slot is about 1. Such a ratio provides the optimum cooling effectiveness.
Document ID
19720051827
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Boldman, D. R.
Papell, S. S.
Ehlers, R. C.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 6, 2013
Publication Date
July 1, 1972
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 9
Subject Category
Thermodynamics And Combustion
Accession Number
72A35493
Distribution Limits
Public
Copyright
Other

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