Modeling of propellants containing ultrafine aluminum

Journal of Propulsion and Power

Volumn 23, Issue 1, 2007, Pages 158-165

  Jackson, T L ^a   Buckmaster, J ^a   Wang, X ^a  

^a UNIVERSITY OF ILLINOIS AT URBANA CHAMPAIGN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM; COMPUTER SIMULATION; FLAMMABILITY; MATHEMATICAL MODELS; PYROLYSIS; THERMAL CONDUCTIVITY;

AMMONIUM PERCHLORATE; GAS PHASE; HOMOGENIZED BLENDS; ULTRA-FINE ALUMINUM;

PROPELLANTS;

EID: 33847013732     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.17493     Document Type: Article

References (14)

1. Jackson, T. L., and Buckmaster, J., "Heterogeneous Propellent Combustion," AIAA Journal, Vol. 40, No. 6, 2002, pp. 1122-1130.
2. Massa, L., Jackson, T. L., Buckmaster, J., and Campbell, M., "Three-Dimensional Heterogeneous Propellant Combustion," Proceedings of the Combustion Institute, Vol. 29, No. 2, 2002, pp. 2975-2983.
3. Massa, L., Jackson, T. L., and Buckmaster, J., "New Kinetics for a Model of Heterogeneous Propellant Combustion," Journal of Propulsion and Power, Vol. 21, No. 5, 2005, pp. 914-924.
4. Sethian, J. A., Level Set Methods and Fast Marching Methods, Cambridge Monograph on Applied and Computational Mathematics, Cambridge Univ. Press, Cambridge, England, U.K., 1999.
5. Osher, S., and Fedkiw, R., Level Set Methods and Dynamic Implicit Surfaces, Vol. 153, Applied Mathematical Sciences, Springer, New York, 2003.
6. Wang, X., Jackson, T. L., and Massa, L., "Numerical Simulation of Heterogeneous Propellant Combustion by a Level Set Method," Combustion Theory and Modeling, Vol. 8, No. 2, 2004, pp. 227-254.
7. Wang, X., and Jackson, T. L., "The Numerical Simulation of Two-Dimensional Aluminized Composite Solid Propellant Combustion," Combustion Theory and Modeling, Vol. 9, No. 1, 2005, pp.171-197.
8. Chen, M., Buckmaster, J., Jackson, T. L., and Massa, L., "Homogenization Issues and the Combustion of Heterogeneous Solid Propellants," Proceedings of the Combustion Institute, Vol. 29, No. 22002, pp. 2923-2929.
9. Dokhan, A., Price, E. W., Seitzman, J. M., and Sigman, R. K., "The Ignition of Ultra-Fine Aluminum in Ammonium Perchlorate Solid Propellant Flames," AIAA Paper 2003-4810, July 2003.
10. Beckstead, M. W., Derr, R. L., and Price, C. F., "Model of Composite Solid-Propellant Combustion Based on Multiple Flames," AIAA Journal, Vol. 8, No. 12, 1970, pp. 2200-2207.
11. Rasmussen, B., and Frederick, R. A., Jr., "A Nonlinear Heterogeneous Model of Composite Solid Propellant Combustion," Journal of Propulsion and Power, Vol. 18, No. 5, 2002, pp. 1086-1092.
12. Ishihara, A., Brewster, M. Q., Sheridan, T. A., and Krier, H., "The Influence of Radiative Heat Feedback on Burning Rates in Aluminized Propellants," Combustion and Flame, Vol. 84, No. 1, 1991, pp. 141-153.
13. Modest, M. F., Radiative Heat Transfer, McGraw-Hill, New York, 1993.
14. Brewster, M. Q., and Parry, D. L., "Radiative Heat Feedback in Aluminized Solid Propellant Combustion," Journal of Thermophysics and Heat Transfer, Vol. 2, No. 2, 1998, pp. 123-130.