Calculation of inviscid supersonic flow over ablated nosetips
- 15 January 1979
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Three-dimensional body-fitted coordinate systems for numerical solution of the Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Aerodynamics of Ballistic Re-entry Vehicles with Asymmetric NosetipsJournal of Spacecraft and Rockets, 1978
- Hypersonic flow over indented nosetipsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977