Fully three-dimensional separated flows computed with the Euler equations
- 24 March 1987
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Flat plate delta wing separated flows with zero total pressure lossesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Numerical simulation of vortical flow over an elliptical-body missile at high angles of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
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- Supersonic conical separation due to shock vorticityAIAA Journal, 1984
- Supersonic Nonlinear Potential Flow with Implicit Isentropic Shock FittingAIAA Journal, 1982