An efficient method for supersonic viscous flow field calculations
- 10 January 1983
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Inviscid Flowfield Calculations for Re-entry Vehicles with Control SurfacesAIAA Journal, 1977
- Multishocked, Three-Dimensional Supersonic Flowfields with Real Gas EffectsAIAA Journal, 1973
- Viscous flow over a cone at moderate incidence—IComputers & Fluids, 1973