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Thermodynamic equilibrium-air correlations for flowfield applicationsEquilibrium-air thermodynamic correlations have been developed for flowfield calculation procedures. A comparison between the postshock results computed by the correlation equations and detailed chemistry calculations is very good. The thermodynamic correlations are incorporated in an approximate inviscid flowfield code with a convective heating capability for the purpose of defining the thermodynamic environment through the shock layer. Comparisons of heating rates computed by the approximate code and a viscous-shock-layer method are good. In addition to presenting the thermodynamic correlations, the impact of several viscosity models on the convective heat transfer is demonstrated.
Document ID
19810036319
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Zoby, E. V.
(NASA Langley Research Center Hampton, VA, United States)
Moss, J. N.
(NASA Langley Research Center Aerodynamics Branch, Space Systems Div., Hampton, Va., United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1981
Subject Category
Thermodynamics And Statistical Physics
Report/Patent Number
AIAA PAPER 81-0280
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: St. Louis, MO
Start Date: January 12, 1981
End Date: January 15, 1981
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
81A20723
Distribution Limits
Public
Copyright
Other

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