Computations of supersonic flows over a body at high angles of attack
- 1 April 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 27 (4), 427-437
- https://doi.org/10.2514/3.10130
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Supercomputing of Supersonic Flows Using Upwind Relaxation and MacCormack SchemesJournal of Fluids Engineering, 1988
- Navier-Stokes computations of prolate spheroids at angle of attackPublished 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
- Computation of turbulent supersonic flows around pointed bodies having crossflow separationJournal of Computational Physics, 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
- Pressures Around an Inclined Ogive Cylinder with Laminar, Transitional, or Turbulent SeparationAIAA Journal, 1982
- Navier-Stokes Solution of a Slender Body of Revolution at IncidenceAIAA Journal, 1982