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A relaxation method for calculating transonic flows with detached bow shocksThe use of Murman and Krupp's (1971) method for calculating steady, inviscid, transonic flows with imbedded shock waves is discussed in application to two-dimensional problems for transonic flows past sharp and moderately blunt nosed geometries. A relaxation algorithm is used to solve the equations.
Document ID
19740034220
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Murman, E. M. (NASA Ames Research Center Moffett Field, Calif., 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
74A16970
Distribution Limits
Public
Copyright
Other

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