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Comparisons between DSMC and the Navier-Stokes equations for reentry flowsA detailed comparison is made between Navier-Stokes and DSMC calculations for flows near the continuum limit to assess the accuracy of the continuum equations in this regime. Meaningful comparisons require the use of similar physical models. This necessitates the inclusion of a separate rotational energy equation and use of slip boundary conditions. Inclusion of slip boundary conditions resulted in improved agreement between surface properties. Moreover, good agreement was obtained for the various temperatures in the nonequilibrium portion of the flow field that does not contain the shock region. Departures are noted in the shock region and in regions where thermal diffusion effects are important.
Document ID
19930062552
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Olynick, David R.
(NASA Ames Research Center Moffett Field, CA, United States)
Taylor, Jeff C.
(NASA Ames Research Center Moffett Field, CA, United States)
Hassan, H. A.
(North Carolina State Univ. Raleigh, United States)
Date Acquired
August 16, 2013
Publication Date
July 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 93-2810
Meeting Information
Meeting: AIAA, Thermophysics Conference
Location: Orlando, FL
Country: United States
Start Date: July 6, 1993
End Date: July 9, 1993
Sponsors: AIAA
Accession Number
93A46549
Funding Number(s)
CONTRACT_GRANT: NCC1-112
CONTRACT_GRANT: NAGW-1331
Distribution Limits
Public
Copyright
Other

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