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Higher-order viscous shock-layer solutions for high altitude flowsA higher-order viscous shock-layer (HVSL) method has been developed and is used to obtain physically consistent results under varying degrees of low-density conditions for perfect-gas and nonequilibrium flows past long slender bodies. This method is implemented with higher-order body and shock slip conditions. Detailed comparisons with the direct simulation Monte Carlo (DSMC) method and Navier-Stokes (NS) calculations establish HVSL as a computationally efficient code for the low-density calculations. Further, it is shown that the deficiencies in the standard viscous shock-layer (VSL) method when predicting low-density flows lie in the governing equations and not with the slip boundary conditions as considered by earlier researchers.
Document ID
19930057053
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gupta, Roop N.
(NASA Langley Research Center Hampton, VA, United States)
Nayani, Sudheer N.
(NASA Langley Research Center Hampton, VA, United States)
Lee, Kam-Pui
(Vigyan, Inc. Hampton, VA, United States)
Zoby, Ernest V.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 16, 2013
Publication Date
July 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 93-2724
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
93A41050
Distribution Limits
Public
Copyright
Other

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