An efficient coordinate transformation technique for unsteady, transonic aerodynamic analysis of low aspect-ratio wings
- 14 May 1984
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- An implicit conservative algorithm for steady and unsteady three-dimensional transonic potential flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- A perturbation method for transonic flows about oscillating airfoilsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975