Numerical experiment with inviscid vortex-stretched flow around a cranked delta wing - Subsonic speed
- 17 August 1985
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Computation of flow around wings based on the Euler equationsJournal of Fluid Mechanics, 1984
- Generation of boundary-conforming grids around wing-body configurations using transfinite interpolationAIAA Journal, 1982
- On the curvature and torsion of an isolated vortex filamentJournal of Fluid Mechanics, 1965