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Abstract: "This paper traces the development of computational fluid dynamics as a tool for aircraft design. It addresses the requirements for effective industrial use, and trade-offs between modeling accuracy and computational costs. Essential elements of algorithm design are discussed in detail, together with a unified approach to the design of shock capturing schemes. Finally, the paper discusses the use of techniques drawn from control theory to determine optimal aerodynamic shapes. In the future multidisciplinary analysis and optimization should be combined to provide an integrated design environment."
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Essential elements of computational algorithms for aerodynamic analysis and design
1997, Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
in English
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Book Details
Edition Notes
"Prepared for Langley Research Center under contracts NAS1-97046 & NAS1-19480, December 1997."
Includes bibliographical references.
Supported in part by the Institute for Computer Applications in Science and Engineering (ICASE) and the National Aeronautics and Space Administration (NASA). NAS1-19480 ; NAS1-97046
Supported in part by the AFOSR. AFOSR 91-0391
Supported in part by ARPA. N00014-92-J-1976
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