Flat plate delta wing separated flows with zero total pressure losses
- 24 March 1987
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Fully three-dimensional separated flows computed with the Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Euler solutions of transonic vortex flows around the Dillner wing - Compared and analyzedPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Supersonic conical separation due to shock vorticityAIAA Journal, 1984
- The λ-schemeComputers & Fluids, 1979