Modeling Multiphase Effects in the Combustion of HMX and RDX
Author:
Affiliation:
1. Naval Air Warfare Center Weapons Division, China Lake, California 93555
2. Brigham Young University, Provo, Utah 84602
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.12689
Reference51 articles.
1. The A Physical Theory of Burning of Double-Base Rocket Propellants. I.
2. The The Theory of the Burning of Double-Base Rocket Powders.
3. The An Hypothesis for Propellant Burning.
4. A Model of Composite Propellant Combustion Including Surface Heterogeneity and Heat Generation
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