An inverse transonic wing design method
- 14 January 1980
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Recent progress in finite-volume calculations for wing-fuselage combinationstransonic potential flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Computational optimization and wind tunnel test of transonic wing designsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Computational transonic design procedure for three-dimensional wings and wing-body combinationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Wing design by numerical optimizationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Theory of viscous transonic flow over airfoils at high Reynolds numberPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Numerical calculation of the transonic flow past a swept wing. [FLO 22]Published by Office of Scientific and Technical Information (OSTI) ,1977
- Calculation of transonic wing flows by grid embeddingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Accelerated iterative calculation of transonic nacelle flowfieldsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Supercritical Wing Sections IIPublished by Springer Nature ,1975
- A rapid computer aided transonic airfoil design methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974