NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
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
19880016075
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Harloff, G. J. (Sverdrup Technology, Inc. Cleveland, OH, United States)
Lai, H. T. (Sverdrup Technology, Inc. Cleveland, OH, United States)
Nelson, E. S. (Sverdrup Technology, Inc. Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1988
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:182150
NASA-CR-182150
E-4190
Accession Number
88N25459
Funding Number(s)
PROJECT: RTOP 505-62-21
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available