Euler equation analysis of the initial roll-up of aircraft wakes
- 6 January 1986
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Three-dimensional unsteady Euler equations solution using flux vector splittingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Multigrid solution of the Euler equations for aircraft configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- A higher order panel method applied to vortex sheet roll-upAIAA Journal, 1983
- Wind-Tunnel Studies of Wing Wake TurbulenceJournal of Aircraft, 1972