Navier-Stokes computations of lee-side flows over delta wings
- 12 May 1986
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Euler and Navier-Stokes solutions for flow over a conical delta wingAIAA Journal, 1986
- Leading-edge separations and cross-flow shocks on delta wingsAIAA Journal, 1985
- Possible Types of Flow at Swept Leading EdgesAeronautical Quarterly, 1964