Supersonic wing and wing-body shape optimization using an adjoint formulation
By: James Reuther and Antony Jameson.
Contributors: Jameson, Antony, 1934-; Research Institute for Advanced Computer Science (U.S.)
Series: NASA contractor report -- NASA CR-199150.; RIACS technical report -- 95.14.; RIACS technical report -- TR 95-14.
Publisher: Research Institute for Advanced Computer Science, NASA Ames Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: [Moffett Field, Calif.]; [Springfield, Va
Language: eng
Format: Microform
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.
Other titles: Supersonic wing and wing body shape optimization using an adjoint formulation.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0195-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.