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Swept-slot film-cooling effectiveness in hypersonic turbulent flowMeasurement results are presented for the surface equilibrium temperature downstream of swept slots, with sonic tangential air injection into a thick hypersonic turbulent boundary layer. These results are compared with unswept slot results for cooling effectiveness.
Document ID
19740046873
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hefner, J. N.
Cary, A. M., Jr. (NASA Langley Research Center Hypersonic Vehicles Div., Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
May 1, 1974
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 11
Subject Category
Thermodynamics And Combustion
Accession Number
74A29623
Distribution Limits
Public
Copyright
Other

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