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