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Computational aerodynamicsThe application of computer techniques for solving Navier-Stokes equations in support of wind tunnel tests is discussed. The ILLIAC IV computer is considered for this purpose and its limitations are analyzed. The author states that improved computers will make it possible to solve many aerodynamic problems and reduce the amount of wind tunnel testing required for adequate data processing.
Document ID
19750020940
Document Type
Conference Paper
Authors
Chapman, D. R. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: NASA/Univ. Conf. on Aeron.
Subject Category
AERODYNAMICS
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19750020928Analytic PrimaryNASA/University Conference on Aeronautics
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