Turbulent base flow on an axisymmetric body with a single exhaust jet
- 1 July 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 7 (7) , 848-854
- https://doi.org/10.2514/3.30052
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- A theory for two-dimensional supersonic turbulent base flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- The Effect of Sting Diameter and Length on Base Pressure at M = 3·88Aeronautical Quarterly, 1968
- An Approximate Theory for Developing Turbulent Free Shear LayersJournal of Basic Engineering, 1967
- Turbulent Mixing of a Rocket Exhaust Jet With a Supersonic Stream Including Chemical ReactionsJournal of the Aerospace Sciences, 1962