A Karhunen-Loeve Galerkin Technique with Shock Fitting for Optimization of a Blunt Body Geometry
- 7 July 2002
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 36 references indexed in Scilit:
- Trust region model management in multidisciplinary design optimizationJournal of Computational and Applied Mathematics, 2000
- Aerodynamic shape optimization of supersonic aircraft configurations via an adjoint formulation on distributed memory parallel computersComputers & Fluids, 1999
- Framework for Multidisciplinary Design Based on Response-Surface ApproximationsJournal of Aircraft, 1999
- Constrained Multipoint Aerodynamic Shape Optimization Using an Adjoint Formulation and Parallel Computers, Part 1Journal of Aircraft, 1999
- Re-Engineering the Design Process Through ComputationJournal of Aircraft, 1999
- Computational Aerothermodynamic Design Issues for Hypersonic VehiclesJournal of Spacecraft and Rockets, 1999
- Model reduction for optimization of rapid thermal chemical vapor deposition systemsIEEE Transactions on Semiconductor Manufacturing, 1998
- Spectral methods for the Euler equations. I - Fourier methods and shock capturingAIAA Journal, 1985
- A Blunt Body in a Supersonic StreamAnnual Review of Fluid Mechanics, 1976
- Optimal Control of Systems Governed by Partial Differential EquationsPublished by Springer Nature ,1971