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Two-dimensional viscous flow computations of hypersonic scramjet nozzle flowfields at design and off-design conditionsThe PARC2D code has been selected to analyze the flowfields of a representative hypersonic scramjet nozzle over a range of flight conditions from Mach 3 to 20. The flowfields, wall pressures, wall skin friction values, heat transfer values and overall nozzle performance are presented.
Document ID
19880063558
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Harloff, G. J. (NASA Lewis Research Center Cleveland, OH, United States)
Lai, H. T. (NASA Lewis Research Center Cleveland, OH, United States)
Nelson, E. S. (NASA Lewis Research Center; Sverdrup Technology, Inc. Cleveland, OH, United States)
Date Acquired
August 13, 2013
Publication Date
July 1, 1988
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 88-3280
Accession Number
88A50785
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Other

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