Navier-Stokes simulation of burst vortex flowfields for fighter aircraft at high incidence
- 1 October 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 28 (10) , 638-645
- https://doi.org/10.2514/3.46076
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Numerical simulation of vortical flows over a strake-delta wingAIAA Journal, 1989
- Navier-Stokes simulations of supersonic fighter intake flowfieldsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Simulation of external flowfields using a three-dimensional Euler/Navier-Stokes algorithmPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Implicit TVD schemes for hyperbolic conservation laws in curvilinearcoordinatesAIAA Journal, 1987
- Simulation of engine installation flowfields using a three-dimensional Euler/Navier-Stokes algorithmPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Navier-Stokes computations of lee-side flows over delta wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Numerical simulation of leading-edge vortex flowsAIAA Journal, 1986
- Comparison of computations and experimental data for leading edge vortices - Effects of yaw and vortex flapsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986