The effect of modeled turbulence on a hypersonic shock layer with massive ablation injection
- 23 June 1981
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Significance of turbulence and transition location on radiative heating with ablation injectionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Nonsimilar Solution for Laminar and Turbulent Boundary-Layer Flows over Ablating SurfacesAIAA Journal, 1972