The Mach disc in underexpanded exhaust plumes
- 19 January 1970
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- DETERMINATION OF HYPERSONIC FLOW FIELDS BY THE METHOD OF CHARACTERISTICSAIAA Journal, 1963
- LOCATION OF THE NORMAL SHOCK WAVE IN THE EXHAUST PLUME OF A JETAIAA Journal, 1963