Computation of steady and unsteady vortex-dominated flows with shockwaves
- 1 May 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 26 (5) , 524-531
- https://doi.org/10.2514/3.9929
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Influence of numerical dissipation on computational Euler equations for vortex-dominated flowsAIAA Journal, 1987
- Finite-volume Euler and Navier-Stokes solvers for three-dimensional and conical vortex flows over delta wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Incompressible Navier-Stokes solutions for a sharp-edged double-delta wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Navier-Stokes computations of vortical flows over low aspect ratio wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Total pressure loss in vortical solutions of the conical Euler equationsAIAA Journal, 1987
- Navier-Stokes computations of lee-side flows over delta wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Euler and Navier-Stokes solutions for flow over a conical delta wingAIAA Journal, 1986
- Numerical simulation of leading-edge vortex flowsAIAA Journal, 1986
- Numerical simulation of vortical flow over an elliptical-body missile at high angles of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Three-dimensional solutions to the Euler equations with one million grid pointsAIAA Journal, 1985