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Navier-Stokes computations useful in aircraft designLarge scale Navier-Stokes computations about aircraft components as well as reasonably complete aircraft configurations are presented and discussed. Speed and memory requirements are described for various general problem classes, which in some cases are already being used in the industrial design environment. Recent computed results, with experimental comparisons when available, are included to highlight the presentation. Finally, prospects for the future are described and recommendations for areas of concentrated research are indicated. The future of Navier-Stokes computations is seen to be rapidly expanding across a broad front of applications, which includes the entire subsonic-to-hypersonic speed regime.
Document ID
19900040256
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Holst, Terry L.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 14, 2013
Publication Date
February 1, 1990
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 90-1800
Accession Number
90A27311
Distribution Limits
Public
Copyright
Other

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