Aerodynamic design optimization via reduced Hessian SQP with solution refining
By: Dan Feng and Thomas H. Pulliam.
Contributors: Pulliam, Thomas H.; Research Institute for Advanced Computer Science (U.S.)
Series: RIACS technical report -- 95-24.; [NASA contractor report] -- NASA-CR-203261.; RIACS technical report -- TR-95-24.; NASA contractor report -- NASA CR-203261.
Publisher: Research Institute for Advanced Computer Science, NASA Ames Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamics.; Optimization.; Nozzle design.; Design analysis.
Notes: Shipping list no.: 98-1104-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.