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Cooling by discrete and porous injection into a turbulent, supersonic boundary layerA summary is provided of an experimental investigation which was carried out to determine the cooling effectiveness of an injection of water through slotted and porous surfaces into a turbulent, supersonic boundary layer. Correlations, based on the experimental data and the supporting analysis, were incorporated into a computer-code model. The model is used to compute discrete injection coolant flow rate requirements for arbitrary slot sizes and heating environments.
Document ID
19740036022
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Clark, K. J.
Nardo, C. T.
Jaffe, N. A. (Acurex Corp. Mountain View, Calif., United States)
Covington, M. A. (NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1974
Subject Category
Fluid Mechanics
Report/Patent Number
AIAA PAPER 74-98
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Washington, DC
Start Date: January 30, 1974
End Date: February 1, 1974
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A18772
Funding Number(s)
CONTRACT_GRANT: F04701-71-C-0087
Distribution Limits
Public
Copyright
Other

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