A Theory of Unstable Combustion in Liquid Propellant Rocket Systems
- 1 September 1951
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the American Rocket Society
- Vol. 21 (5), 108-114
- https://doi.org/10.2514/8.4374
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Stability of Flow in a Rocket MotorJournal of Applied Mechanics, 1950
- Self-Excited Oscillations in Dynamical Systems Possessing Retarded ActionsJournal of Applied Mechanics, 1942