Combustion Response Function Measurements by the Rotating Valve Method
- 1 November 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (11) , 1502-1510
- https://doi.org/10.2514/3.49536
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- The T-burner test method for determining the combustion response of solid propellantsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Linear and nonlinear pressure coupled combustion instability of solid propellantsAIAA Journal, 1970
- A review of calculations for unsteady burning of a solid propellant.AIAA Journal, 1968
- Surface reaction effects on the acoustic response of composite solidpropellants.AIAA Journal, 1968
- Nonacoustic combustor instability.AIAA Journal, 1967
- An interpretation of L' combustion instability in terms of acoustic instability theory.AIAA Journal, 1967
- Influence of combustion parameters on instability in solid propellant motors. I - Development of model and linear analysis.AIAA Journal, 1966
- Interaction between Sound and Flow in Acoustic Cavities: Mass, Momentum, and Energy ConsiderationsThe Journal of the Acoustical Society of America, 1964
- A Simplified Model of Unstable Burning in Solid PropellantsARS Journal, 1961