An incremental strategy for calculating consistent discrete CFD sensitivity derivatives /

Bibliographic Details
Corporate Authors:	Langley Research Center, United States. Army Aviation Systems Command
Other Authors:	Korivi, Vamshi Mohan
Format:	Government Document Microform Book
Language:	English
Published:	Hampton, VA : [St. Louis, Mo.] : National Aeronautics and Space Administration, Langley Research Center ; US Army Aviation Systems Command, [1992]
Series:	AVSCOM technical report ; 92-B-006. NASA technical memorandum ; 104207.
Subjects:	Aerodynamic characteristics. Aircraft design. Airfoils. Computational fluid dynamics. Computer aided design. Iterative solution. Navier-Stokes equation. Nozzle flow. Sensitivity. Transonic flow.
Online Access:	https://purl.fdlp.gov/GPO/LPS60335

Description
Item Description:	Shipping list number: 92-2230-M. "February 1992." Microform.
Physical Description:	1 volume 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.