Theory of Liquid PropelIant Rocket Combustion Instability and Its Experimental Verification
- 1 February 1960
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in ARS Journal
- Vol. 30 (2), 159-168
- https://doi.org/10.2514/8.5020
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- An Experimental Study of High-Frequency Combustion Pressure OscillationsJournal of Jet Propulsion, 1958
- Dynamic Pressure Measuring Systems for Jet Propulsion ResearchJournal of the American Rocket Society, 1953
- Combustion Studies in Rocket MotorsJournal of the American Rocket Society, 1953
- A Theory of Unstable Combustion in Liquid Propellant Rocket SystemsJournal of the American Rocket Society, 1951
- Discussion: “Stability of Flow in a Rocket Motor” (Gunder, D. F., and Friant, D. R., 1950, ASME J. Appl. Mech., 17, pp. 327–333)Journal of Applied Mechanics, 1951
- Stability of Flow in a Rocket MotorJournal of Applied Mechanics, 1950