Computational optimization and wind tunnel test of transonic wing designs
- 15 January 1979
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Wing design by numerical optimizationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Application of Numerical Optimization to the Design of Supercritical Airfoils without Drag-CreepPublished by SAE International ,1977
- Supercritical Wing Sections IIPublished by Springer Nature ,1975
- Iterative solution of transonic flows over airfoils and wings, including flows at mach 1Communications on Pure and Applied Mathematics, 1974