An investigation of the swirling flow in a spinning end-burning rocket
- 1 December 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (12) , 2293-2300
- https://doi.org/10.2514/3.5530
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- An investigation of the effect of acceleration on the burning rate of composite propellants.AIAA Journal, 1968
- Approximate Solution of Isentropic Swirling Flow Through a NozzleARS Journal, 1961
- SOURCES AND SINKS AT THE AXIS OF A ROTATING LIQUIDThe Quarterly Journal of Mechanics and Applied Mathematics, 1956