Constrained Multipoint Aerodynamic Shape Optimization Using an Adjoint Formulation and Parallel Computers, Part 2
- 1 January 1999
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 36 (1), 61-74
- https://doi.org/10.2514/2.2414
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Constrained Multipoint Aerodynamic Shape Optimization Using an Adjoint Formulation and Parallel Computers, Part 1Journal of Aircraft, 1999
- Constrained multipoint aerodynamic shape optimization using an adjoint formulation and parallel computersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Aerodynamic design optimization on unstructured grids with a continuous adjoint formulationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Automatic aerodynamic optimization on distributed memory architecturesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Optimum aerodynamic design using CFD and control theoryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Multigrid algorithms for compressible flow calculationsLecture Notes in Mathematics, 1986