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Solution of the transonic full potential equation in conservative form using an implicit algorithmThe paper presents numerical solutions of the full potential equation in conservative form. The iteration scheme used is a fully implicit approximate factorization technique and provides a significant improvement in convergence speed relative to standard successive line overrelaxation algorithms. The spatial differencing algorithm is centrally differenced in both subsonic and supersonic regions to maintain stability. This effectively approximates rotated differencing, thereby greatly improving the reliability of the algorithm.
Document ID
19820029069
Acquisition Source
Legacy CDMS
Document Type
Other - Collected Works
Authors
Holst, T.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1981
Subject Category
Aerodynamics
Accession Number
82A12604
Distribution Limits
Public
Copyright
Other

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