An incremental strategy for calculating consistent discrete CFD sensitivity derivatives
By: Vamshi Mohan Korivi ... [et al.].
Contributors: Korivi, Vamshi Mohan.; Langley Research Center.; United States. Army Aviation Systems Command.
Series: NASA technical memorandum -- 104207.; AVSCOM technical report -- 92-B-006.
Publisher: National Aeronautics and Space Administration, Langley Research Center; US Army Aviation Systems Command
Published: 1992
Place of publication: Hampton, VA; [St. Louis, MO]
Language: eng
Format: Microform
Subjects: Aerodynamic characteristics.; Aircraft design.; Airfoils.; Computational fluid dynamics.; Computer aided design.; Iterative solution.; Navier-Stokes equation.; Nozzle flow.; Sensitivity.; Transonic flow.
Notes: Shipping list no.: 92-2230-M.

"February 1992."

Also available via Internet from the NASA Technical Report Server web site. Address as of 5/6/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19920015438%5F1992015438.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1992]. 1 microfiche.