Aerodynamic spike flowfields computed to select optimum configuration at Mach 2.5 with experimental validation
- 8 January 1990
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Modes of shock-wave oscillations on spike-tipped bodiesAIAA Journal, 1985
- Flow Oscillations of Spike-Tipped BodiesAIAA Journal, 1982