Essential elements of computational algorithms for aerodynamic analysis and design
By: Antony Jameson.
Contributors: Institute for Computer Applications in Science and Engineering.; Langley Research Center.
Series: ICASE report -- no. 97-68; NASA/CR -- 97-206268; NASA contractor report -- 97-68.
Publisher: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
Published: 1997
Place of publication: Hampton, Va
Language: eng
Number of pages: 66
Subjects: Aerodynamics -- Mathematical models.; Computer-aided design.; Control theory.; Fluid dynamics -- Mathematical models.
Other titles: ICASE 25th anniversary
Description: 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."
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