Particulate multi-phase flowfield calculation with combustion/breakup models for solid rocket motor
Author:
Affiliation:
1. Engineering Sciences, Inc., Huntsville, AL
2. NASA, Marshall Space Center, Huntsville, AL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-2780
Reference24 articles.
1. Calculation of the two-phase aft-dome flowfield in solid rocket motors
2. Simple modeling of particle trajectories in solid rocket motors
3. Sabnis, J., Jong, F. de, and Gibeling, H. "A Two-PhaseRestricted EquilibriumModel forCombustion of Metalized solid Propellants," AIAA-92-3509.
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