Prediction of subsonic aerodynamic characteristics - A case for low order panel methods
- 12 January 1981
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Calculation of transonic flow by means of a shock-capturing field panel methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979