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Fundamental problem in computing radiating flow fields with thick shock wavesPossible reasons for the failure of the Navier-Stokes equations to yield realistic profiles of the temperature and density through the structure of a hypersonic shock wave are investigated. Models for bulk viscosity in a monatomic gas are examined which yield a realistic thickness for the shock-wave density profile, but not the temperature profile, and hence are not satisfactory. A tentative computational model for nitrogen is explored which yields considerably more realistic results than the Navier-Stokes equations. This model involves a nonlinear stress-strain tensor, nonlinear heat flux vector, and nonequilibrium rotational energy.
Document ID
19890026827
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chapman, Dean R.
(Stanford Univ. CA, United States)
Lumpkin, Forrest E.
(Stanford University CA, United States)
Fiscko, Kurt A.
(U.S. Army, Washington, DC; Stanford University CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1988
Subject Category
Aerodynamics
Meeting Information
Meeting: Sensing, Discrimination, and Signal Processing and Superconducting Materials and Instrumentation
Location: Los Angeles, CA
Country: United States
Start Date: January 12, 1988
End Date: January 14, 1988
Sponsors: SPIE
Accession Number
89A14198
Funding Number(s)
CONTRACT_GRANT: NAGW-965
CONTRACT_GRANT: DAAL03-86-K-0139
Distribution Limits
Public
Copyright
Other

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