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Numerical solutions of the supersonic, laminar flow over a two-dimensional compression cornerNumerical solutions of Navier-Stokes equations are presented for the supersonic laminar flow over a two-dimensional compression corner. A well-known time-dependent method has been used wherein the asymptotic steady solutions of the unsteady Navier-Stokes equations are obtained with the Brailovskaia (1965) finite-difference scheme.
Document ID
19740034206
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Carter, J. E. (NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Subject Category
Aerodynamics
Meeting Information
Meeting: International Conference on Numerical Methods in Fluid Mechanics
Location: Paris
Country: France
Start Date: July 3, 1972
End Date: July 7, 1972
Accession Number
74A16956
Distribution Limits
Public
Copyright
Other

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