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Turbulent viscous-shock-layer solutions with strong vorticity interactionNumerical solutions of the viscous-shock-layer equations governing laminar and turbulent flows of a perfect gas and radiating and nonradiating mixtures of perfect gases in chemical equilibrium are presented for hypersonic flow over spherically blunted cones and hyperboloids. The results are compared with boundary-layer and inviscid flow-field solutions. The agreement with the inviscid flow field data is satisfactory. The agreement with boundary-layer solutions is good except in regions of strong vorticity interaction. In these flow regions, the viscous-shock-layer solutions appear to be more satisfactory than the boundary-layer solutions.
Document ID
19760035839
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Anderson, E. C. (NASA Langley Research Center Hampton, VA, United States)
Moss, J. N. (NASA Langley Research Center Hampton, VA, United States)
Sutton, K. (NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 76-120
Report Number: AIAA PAPER 76-120
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Washington, DC
Start Date: January 26, 1976
End Date: January 28, 1976
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
76A18805
Distribution Limits
Public
Copyright
Other

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