Influence of combustion parameters on instability in solid propellant motors. I - Development of model and linear analysis.
- 1 September 1966
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (9) , 1604-1609
- https://doi.org/10.2514/3.3742
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Linear acoustic gains and losses in solid propellant rocket motorsAIAA Journal, 1964
- Use of the one-dimensional t-burner to study oscillatory combustionAIAA Journal, 1964
- Reply by Author to W.H. AndersenAIAA Journal, 1964
- PARTICULATE DAMPING OF OSCILLATORY COMBUSTIONAIAA Journal, 1963
- A Simplified Model of Unstable Burning in Solid PropellantsARS Journal, 1961
- Effect of Solid Propellant Compressibility on Combustion InstabilityThe Journal of Chemical Physics, 1960
- Solid Propellant Rocket Motors as Acoustic OscillatorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1960
- Combustion Instability: Acoustic Interaction with a Burning Propellant SurfaceThe Journal of Chemical Physics, 1959
- Resonance burning in rocket motorsCommunications on Pure and Applied Mathematics, 1949