Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design
By: E. Carson Yates, Jr.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 102677
Publisher: National Aeronautics and Space Administration, Langley Research Center; For sale by the National Technical Information Service
Published: 1990
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 15
Subjects: Aeroelasticity.; Aeroelasticity.; Computer aided design.; Integral equations.; Inviscid flow.; Supersonics.; Transonic flow.; Unsteady aerodynamics.; Viscous flow.
Notes: Cover title.

"May 1990."

Includes bibliographical references (p. 9-11).

Also available via Internet from the NASA Technical Report Server web site. Address as of 12/16/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900015794%5F1990015794.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative.