Aerodynamic design optimization via reduced Hessian SQP with solution refining [microform] / Dan Feng and Thomas H. Pulliam (RIACS technical report ; 95-24) ([NASA contractor report] ; NASA-CR-203261)
Aerodynamic design optimization via reduced Hessian SQP with solution refining [microform] / Dan Feng and Thomas H. Pulliam
原資料の出版事項: [Washington, DC] ; [Springfield, Va. : Research Institute for Advanced Computer Science, NASA Ames Research Center : National Technical Information Service, distributor, 1995]