The effects of Al particle size on the burning rate and residual oxide in aluminized propellants
Author:
Affiliation:
1. Georgia Inst. of Technology, Atlanta
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-3581
Reference12 articles.
1. Price, E. W., and Sigman, R. K. "Combustion of Aluminized Propellants," Solid Propellant Chemistry, Combustion,andMotor Interior Ballistics,Vol.185 of A1AAProgressseries,2000,pp.663-687.
2. Combustion instabilities - Mating dance of chemical, combustion, and combustor dynamics
3. AlAA-2001-3581
4. Aluminum Agglomeration in Solid-Propellant Combustion
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