A combined direct/inverse three-dimensional transonic wing design method for vector computers
- 17 August 1984
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- A F?LL POTENTIAL INVERSE METHOD BASED ON A DENSITY LINEARIZATION SCHEME FOR WING DESIGNPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Iterative solution of transonic flows over airfoils and wings, including flows at mach 1Communications on Pure and Applied Mathematics, 1974