Aerodynamic design optimization via reduced Hessian SQP with solution refining

An edition of Aerodynamic design optimization via reduced Hessian SQP with solution refining (1995)

Aerodynamic design optimization via reduced Hessian SQP with solution refining

By Dan Feng

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Publish Date

1995

Publisher

Research Institute for Advanced Computer Science, NASA Ames Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Aerodynamics, Optimization, Nozzle design, Design analysis