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HEAT TRANSFER TO AN INCOMPRESSIBLE TURBULENT BOUNDARY LAYER AND ESTIMATION OF HEAT-TRANSFER COEFFICIENTS AT SUPERSONIC NOZZLE THROATS
Document ID
19630042866
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sibulkin, M. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 1, 2013
Publication Date
July 16, 1954
Subject Category
Facilities, Research, And Support
Accession Number
63N85759
Funding Number(s)
CONTRACT_GRANT: DA-04-495-ORD-18
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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