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Test problems for inviscid transonic flowSolving of test problems with the TRANDES program is discussed. This method utilizes the full, inviscid, perturbation potential flow equation in a Cartesian grid system that is stretched to infinity. This equation is represented by a nonconservative system of finite difference equations that includes at supersonic points a rotated difference scheme and is solved by column relaxation. The solution usually starts from a zero perturbation potential on a very coarse grid (typically 13 by 7) followed by several grid halvings until a final solution is obtained on a fine grid (97 by 49).
Document ID
19790021971
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Carlson, L. A.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-162138
TEES-TAMRF-3224-7804
Report Number: NASA-CR-162138
Report Number: TEES-TAMRF-3224-7804
Meeting Information
Meeting: GAMM Workshop on Numerical Methods for the Computation of Inviscid Transonic Flow with Shock Waves
Location: Stockholm
Country: Sweden
Start Date: September 18, 1979
End Date: September 19, 1979
Accession Number
79N30142
Funding Number(s)
CONTRACT_GRANT: NSG-1174
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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