Effect of oxidizer concentration on combustion instability of a solid propellant
- 1 September 1964
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (9) , 1654-1655
- https://doi.org/10.2514/3.2640
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- The effect of compositional variables upon oscillatory combustion of solid rocket propellantsCombustion and Flame, 1964
- VIRTUAL SPECIFIC ACOUSTIC ADMITTANCE MEASUREMENTS OF BURNING SOLID PROPELLANT SURFACES BY A RESONANT TUBE TECHNIQUEPublished by Elsevier ,1963
- Combustion Instability: Acoustic Interaction with a Burning Propellant SurfaceThe Journal of Chemical Physics, 1959