Surface reaction effects on the acoustic response of composite solidpropellants.
- 1 March 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (3), 479-488
- https://doi.org/10.2514/3.4523
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- A DETAILED MODEL OF THE COMBUSTION OF COMPOSITE SOLID PROPELLANTSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- THE EFFECT OF SURFACE REACTIONS ON THE SOLID PROPELLANT RESPONSE FUNCTIONPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- The effect of compositional variables upon oscillatory combustion of solid rocket propellantsCombustion and Flame, 1964
- The t-burner method of determining the acoustic admittance of burning propellantsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1964
- Theory of hypergolic ignition of solid propellantsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1963
- VIRTUAL SPECIFIC ACOUSTIC ADMITTANCE MEASUREMENTS OF BURNING SOLID PROPELLANT SURFACES BY A RESONANT TUBE TECHNIQUEPublished by Elsevier ,1963
- 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
- Burning Rates of Solid PropellantsThe Journal of Chemical Physics, 1960
- The theory of burning of solid and liquid propellantsCombustion and Flame, 1960