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A shock capturing application of the finite element methodThe paper is concerned with the development of finite element algorithms for the solution of viscous compressible flow problems with possible embedded shocks and recirculation regions. As a first step, the calculation in Cartesian coordinates of uniform flow on a rectangular region which encounters an embedded oblique shock with known turning angle is considered. A code is developed which is then used for computation of the boattail plume simulator problem in cylindrical coordinates. Oblique shock calculations are performed and the results are compared with a known finite difference solution.
Document ID
19790040758
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Cooke, C. H.
(Old Dominion University Norfolk, Va., United States)
Blanchard, D. K.
(NASA Langley Research Center High Speed Aerodynamics Div., Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: International Journal for Numerical Methods in Engineering
Volume: 14
Issue: 2, 19
Subject Category
Aerodynamics
Accession Number
79A24771
Funding Number(s)
CONTRACT_GRANT: NSG-1098
Distribution Limits
Public
Copyright
Other

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