Computation of steady and unsteady vortex dominated flows
- 8 June 1987
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Extension and applications of flux-vector splitting to unsteady calculations on dynamic meshesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,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
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- Solution of unsteady rotational flow over supercritical wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Euler solution of the transonic flow for a helicopter rotorPublished 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
- Numerical simulation of leading-edge vortex flowsAIAA Journal, 1986
- Three-dimensional solutions to the Euler equations with one million grid pointsAIAA Journal, 1985
- Total pressure loss in vortical solutions of the conical Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- A comparison of Euler and Navier-Stokes solutions for supersonic flow over a conical delta wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985