Finite acoustic oscillations and erosive burning in solid fuel rockets.
- 1 December 1965
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (12), 2248-2256
- https://doi.org/10.2514/3.3353
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Experimental solid rocket combustion instabilitySymposium (International) on Combustion, 1965
- Effect of acoustic environment on the burning rate of solid propellantsAIAA Journal, 1964
- Nonlinear Effects in Instability of Solid-Propellant Rocket MotorsAIAA Journal, 1964
- Interaction between Sound and Flow in Acoustic Cavities: Mass, Momentum, and Energy ConsiderationsThe Journal of the Acoustical Society of America, 1964
- Nonlinear axial combustion instability in solid propellant motorsAIAA Journal, 1964
- Interaction Between Sound and Flow: Stability of T-BurnersAIAA Journal, 1963
- AMPLIFICATION AND ATTENUATION OF SOUND BY BURNING PROPELLANTSAIAA Journal, 1963
- Erosion Mechanism for Nonlinear Instability in the Axial Modes of Solid Propellant Rocket MotorsARS Journal, 1962
- "Catastrophic" Changes in Burning Rate of Solid Propellants During Combustion InstabilityARS Journal, 1960
- Combustion Instability in Solid Propellant Rocket MotorsPublished by Springer Nature ,1959