Direct simulation of transitional flow for hypersonic reentry conditions
- 9 January 1984
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Viscous-shock-layer heating analysis for the shuttle windward-symmetry plane with surface finite catalytic recombination ratesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Determination of atmospheric properties for STS-1 aerothermodynamic investigationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981