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Finite area method for nonlinear conical flowsA fully conservative finite area method for the computation of steady inviscid flow about general conical bodies at incidence is described. The procedure utilizes the potential approximation and implements a body conforming mesh generator. The conical potential is assumed to have its best linear variation inside each mesh cell and a secondary interlocking cell system is used to establish the flux balance required to conserve mass. In the supersonic regions the scheme is desymmetrized by adding appropriate artificial viscosity in conservation form. The algorithm is nearly an order of a magnitude faster than present Euler methods and predicts known results accurately and qualitative features such as nodal point lift off correctly. Results are compared with those of other investigations.
Document ID
19820053940
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sritharan, S. S.
(Arizona, University Tucson, AZ, United States)
Seebass, A. R.
(Colorado, University Boulder, CO, United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 82-0995
Meeting Information
Meeting: Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference
Location: St. Louis, MO
Start Date: June 7, 1982
End Date: June 11, 1982
Sponsors: American Institute of Aeronautics and Astronautics and American Society of Mechanical Engineers
Accession Number
82A37475
Funding Number(s)
CONTRACT_GRANT: N00014-76-C-0182
CONTRACT_GRANT: NGT-03-002-800
CONTRACT_GRANT: AF-AFOSR-81-0107
Distribution Limits
Public
Copyright
Other

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