The effects of Al particle size on the burning rate and residual oxide in aluminized propellants
- 8 July 2001
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Combustion instabilities - Mating dance of chemical, combustion, and combustor dynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- Combustion of Aluminized Solid PropellantsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- The Details of Combustion of Ammonium Perchlorate Propellants: Leading Edge Flame DetachmentCombustion Science and Technology, 1998
- Means of modifying metallic fuel in condensed systemsCombustion, Explosion, and Shock Waves, 1990
- Aluminum Agglomeration in Solid-Propellant CombustionAIAA Journal, 1984