Effect of surface reactions on the solid propellant response function.
- 1 March 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (3), 471-478
- https://doi.org/10.2514/3.4522
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- A new theoretical solution of the laminar, hypersonic near wake.AIAA Journal, 1967
- Hypersonic boundary-layer separation and the base flow problem.AIAA Journal, 1966
- Rapid expansion of a supersonic boundary layer and its application to the near wake.AIAA Journal, 1966
- Experimental solid rocket combustion instabilitySymposium (International) on Combustion, 1965
- Theory of acoustic instability in solid-propellant rocket combustionSymposium (International) on Combustion, 1965
- Linear acoustic gains and losses in solid propellant rocket motorsAIAA Journal, 1964
- Response of a Burning Solid to Small-Amplitude Pressure OscillationsJournal of Applied Physics, 1962
- A Simplified Model of Unstable Burning in Solid PropellantsARS Journal, 1961
- Acoustic Resonance in Solid Propellant RocketsJournal of Applied Physics, 1960
- Combustion Instability: Acoustic Interaction with a Burning Propellant SurfaceThe Journal of Chemical Physics, 1959