Joint computational experimental aerodynamics research on a hypersonic vehicle. II - Computational results
- 7 January 1991
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Accurate Navier-Stokes results for the hypersonic flow over a spherical nosetipPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Evaluation of PNS-computed heating and hypersonic shock tunnel data on sharp and inclined blunt conesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Comparisons of Monte-Carlo and PNS calculations for rarefied flow over reentry vehicle configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Evaluation of boundary-layer and parabolized Navier-Stokes solutionsfor re-entry vehiclesJournal of Spacecraft and Rockets, 1986
- Computation of hypersonic viscous flow around three-dimensional bodies at high angles of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981