Supersonic wing and wing-body shape optimization using an adjoint formulation [microform] / James Reuther and Antony Jameson.

Saved in:

Bibliographic Details
Main Author:	Reuther, James
Corporate Author:	Research Institute for Advanced Computer Science (U.S.)
Other Authors:	Jameson, Antony, 1934-
Other title:	Supersonic wing and wing body shape optimization using an adjoint formulation.
Format:	Government Document Microfilm Book
Language:	English
Published:	[Moffett Field, Calif.] : [Springfield, Va.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [National Technical Information Service, distributor], [1995]
Series:	RIACS technical report ; TR 95-14. NASA contractor report ; NASA CR-199150.
Subjects:	Aerodynamic configurations. Aircraft design. Body-wing configurations. Computational fluid dynamics. Control theory. Euler equations of motion. Optimization. Supersonic aircraft. Supersonic airfoils. Supersonic flow. Three dimensional flow. Wings.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:199150
NAS 1.26:199150	Restricted Place a Hold