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Implicit, nonswitching, vector-oriented algorithm for steady transonic flowA rapid computation of a sequence of transonic flow solutions has to be performed in many areas of aerodynamic technology. The employment of low-cost vector array processors makes the conduction of such calculations economically feasible. However, for a full utilization of the new hardware, the developed algorithms must take advantage of the special characteristics of the vector array processor. The present investigation has the objective to develop an efficient algorithm for solving transonic flow problems governed by mixed partial differential equations on an array processor.
Document ID
19840027360
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Lottati, I.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
November 1, 1983
Publication Information
Publication: AIAA Journal
Volume: 21
ISSN: 0001-1452
Subject Category
Aerodynamics
Accession Number
84A10147
Distribution Limits
Public
Copyright
Other

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