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International Journal of Energetic Materials and Chemical Propulsion
Редактор-основатель: Kenneth K. Kuo (open in a new tab)

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ISSN Печать: 2150-766X

ISSN Онлайн: 2150-7678

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UNDERSTANDING THE BURNING OF HETEROGENEOUS SOLID PROPELLANTS THROUGH MESOSCALE MODELING

Том 20, Выпуск 2, 2021, pp. 67-86
DOI: 10.1615/IntJEnergeticMaterialsChemProp.2021037525
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Stany Gallier
ArianeGroup, 9 Rue Lavoisier, Vert le Petit, 91710, France
Mathieu Plaud
ArianeGroup, Vert le Petit, 91710, France

Краткое описание

Heterogeneous solid propellants are widely used in the rocket industry. They consist of oxidizer particles embedded in a polymeric binder. The combustion and ignition of such propellants remain poorly understood, partly because they are complex and driven by physical mechanisms occurring at the micrometer scale. This paper gives an overview of some recent achievements in understanding the physics of propellant burning using mesoscale direct simulations. In this modeling, the propellant microstructure is explicitly modeled, and basic governing equations (reactive Navier-Stokes equations) are solved in three dimensions at the subparticle level. Most present findings suggest a salient role of propellant microstructure. This is the case for steady combustion where the orientation of particles (assumed as spheroids) has a strong impact on burn rate, while particle shape has a more limited effect. Ignition can also be addressed; it is found that ignition physics is strongly related to particles on the surface, like flame spreading from ignited particles. Mesoscale simulations can be part of a more general multiscale strategy applied to real motors. Two applications are discussed: the first is related to the effects of the grain manufacturing process on burning rate, and the second focuses on how local small-scale burning fluctuations above the propellant surface can trigger flow instabilities in a motor. This strengthens the interest of mesoscale modeling, both for understanding physics and predicting actual systems.

Ключевые слова: heterogeneous propellant, combustion, microstructure, ignition, mesoscale simulation, ammonium perchlorate
ЛИТЕРАТУРА

  1. Beckstead, M., Overview of Combustion Mechanisms and Flame Structures for Advanced Solid Propellants, in Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics, V. Yang, T. Brill, W.Z. Ren, Eds., vol. 185, pp. 267-286,2000.

  2. Beckstead, M.W., Recent Progress in Modeling Solid Propellant Combustion, Combust., Expl. Sh. Waves, vol. 42, no. 6, pp. 623-641,2006.

  3. Beckstead, M.W., Derr, R., and Price, C., A Model of Composite Solid-Propellant Combustion Based on Multiple Flames, AIAA J., vol. 8, no. 12, pp. 2200-2207, 1970.

  4. Beyer, R., Anderson, R., MacLaren, R., and Corcoran, W., Ignition of Solid-Propellant Motors under Vacuum, United Technology Center, Sunnyvale, CA, Final Rep. No. UTC-2079-FR, p. 9701,1965.

  5. Buckmaster, J., Wang, X., and Jackson, T., Burning of Ammonium-Perchlorate Ellipses and Spheroids in Fuel Binder, J. Prop. Power, vol. 22, no. 4, pp. 764-768,2006.

  6. Cai, W., Ma, F., and Yang, V., Two-Phase Vorticoacoustic Flow Interactions in Solid-Propellant Rocket Motors, J. Prop. Power, vol. 19, no. 3, pp. 385-396,2003.

  7. Chedevergne, F., Casalis, G., and Majdalani, J., Direct Numerical Simulation and Biglobal Stability Investigations of the Gaseous Motion in Solid Rocket Motors, J. Fluid Mech, vol. 706, no. 1, pp. 190-218, 2012.

  8. Chen, M., Buckmaster, J., Jackson, T., and Massa, L., Homogenization Issues and the Combustion of Heterogeneous Solid Propellants, Proc. Combust. Inst., vol. 29, no. 2, pp. 2923-2929,2002.

  9. Davidson, L., Hybrid LES-RANS: Inlet Boundary Conditions for Flows with Recirculation, in Advances in Hybrid RANS-LES Modeling, New York, NY: Springer, 2008.

  10. DeLuca, L., Ohlemiller, T., Caveny, L., and Summerfield, M., Radiative Ignition of Double Base Propellants. II-Pre-Ignition Events and Source Effects, AIAA J., vol. 14, no. 8, pp. 1111-1117,1976.

  11. Durand, P., Vieille, B., Lambare, H., Vuillermoz, P., Boure, G., Steinfeld, P., Godfroy, F., and Guery, J., CPS: A Three-Dimensional CFD Numerical Code Dedicated to Space Propulsive Flows, AIAA Paper 2000-3864,2000.

  12. Fabignon, Y., Dupays, J., Avalon, G., Vuillot, F., Lupoglazoff,N., Casalis, G., andPrevost, M., Instabilities and Pressure Oscillations in Solid Rocket Motors, Aerosp. Sci. Tech., vol. 7, no. 3, pp. 191-200,2003.

  13. Francois, G., Ville, L., and Gallier, S., 3D Simulation Model for Highly Loaded Fluids with Large Spherical Particles, The 12th Int. Conf. on Numerical Methods in Industrial Forming Processes (NUMIFORM-2016), Troyes, France, July 4-7,2016.

  14. Gallier, S., Ferrand, A., and Plaud, M., Three-Dimensional Simulations of Ignition of Composite Solid Propellants, Combust. Flame, vol. 173, pp. 2-15,2016.

  15. Gallier, S. and Plaud, M., A Model for Solid Propellant Burning Fluctuations Using Mesoscale Simulations, Acta Astronaut., vol. 158, pp. 296-303,2019a.

  16. Gallier, S. and Plaud, M., Vorticoacoustic Stability of Solid Rocket Motors: a Numerical Study, J. Prop. Power, vol. 35, no. 4, pp. 787-801,2019b.

  17. Gallier, S. and Plaud, M., Effect of Particle Orientation on the Burning Rate of Ammonium Perchlorate Solid Propellants, Comb. Explos. Sh. Waves, 2021. (accepted).

  18. Gallier, S., Prevost, M., Hijlkema, J., and Roumy, M., Effects of Cavity on Thrust Oscillations in Subscale Solid Rocket Motors, in 45th AIAA/ASME/SAE/ASEE Joint Propuls. Conf. Exhibit, AIAA Paper 2009-5253, 2009.

  19. Genot, A., Gallier, S., and Schuller, T., Model for Acoustic Induced Aluminum Combustion Fluctuations in Solid Rocket Motors, J. Prop. Power, vol. 35, no. 4, pp. 720-735,2019.

  20. Gross, M.L. and Beckstead, M.W., Steady-State Combustion Mechanisms of Ammonium Perchlorate Composite Propellants, J. Prop. Power, vol. 27, no. 5, pp. 1064-1078,2011.

  21. Gross, M.L., Hedman, T.D., Son, S.F., Jackson, T.L., and Beckstead, M.W., Coupling Micro and Meso-Scale Combustion Models of AP/HTPB Propellants, Combust. Flame, vol. 160, no. 5, pp. 982-992, 2013.

  22. Guery, J., Godfroy, F., Ballereau, S., Gallier, S., Della Pieta, P., Orlandi, O., Robert, E., and Cesco, N., Thrust Oscillations in Solid Rocket Motors, in 44th AIAA/ASME/SAE/ASEE Joint Propuls. Conf. Exhibit, AIAA Paper 2008-4979,2008.

  23. Heister, S., Ballistics of Solid Rocket Motors with Spatial Burning Rate Variations, J. Prop. Power, vol. 9, no. 4, pp. 649-651,1993.

  24. Jackson, T. and Buckmaster, J., Heterogeneous Propellant Combustion, AIAA J, vol. 40, no. 6, pp. 1122-1130,2002.

  25. Jodrey, W. and Tory, E., Computer Simulation of Close Random Packing of Equal Spheres, Phys. Rev. A, vol. 32, no. 4, p. 2347,1985.

  26. Kallmeyer, T. and Sayer, L., Differences between Actual and Predicted Pressure-Time Histories of Solid Rocket Motors, in 18th Joint Propuls. Conf., AIAA Paper 82-1094,1982.

  27. Kitagawa, K., Shimada, T., Hasegawa, H., Fukunaga, M., Miyachi, H., and Kosuge, H., Correlation of Midweb Anomaly with Microstructure of Composite Propellant Containing High Amount of Aluminum, in 47th AIAA/ASME/SAE/ASEE Joint Propuls. Conf. Exhibit, AIAA Paper 2011-5714,2011.

  28. Le Breton, P. and Ribereau, D., Casting Process Impact on Small-Scale Solid Rocket Motor Ballistic Per-formance, J. Prop. Power, vol. 18, no. 6, pp. 1211-1217,2002.

  29. Leighton, D. and Acrivos, A., The Shear-Induced Migration of Particles in Concentrated Suspensions, J. FluidMech., vol. 181, pp. 415-439,1987.

  30. Massa, L., Jackson, T., and Buckmaster, J., New Kinetics for a Model of Heterogeneous Propellant Combustion, J. Prop. Power, vol. 21, no. 5, pp. 914-924,2005.

  31. Massa, L., Jackson, T., Buckmaster, J., and Najj ar, F., Fluctuations above a Burning Heterogeneous Propellant, J. Fluid Mech, vol. 581, pp. 1-32,2007.

  32. Massa, L., Jackson, T., and Short, M., Numerical Solution of Three-Dimensional Heterogeneous Solid Propellants, Combust. Theor. Model., vol. 7, no. 3, pp. 579-602,2003.

  33. Mercier, R., Lacassagne, L., and Plaud, M., A Tabulated Chemistry Method for Heterogeneous Solid Propellant Combustion, Proc. Combus. Inst., vol. 38, no. 3, pp. 4425-4432,2021.

  34. Miller, R., Effects of Particle Size on Reduced Smoke Propellant Ballistics, in 18th Joint Propuls. Conf, AIAA Paper 82-1096,1982.

  35. Morris, J.F. and Boulay, F., Curvilinear Flows of Noncolloidal Suspensions: The Role of Normal Stresses, J. Rheol., vol. 43, no. 5, pp. 1213-1237,1999.

  36. Plaud, M., Gallier, S., and Morel, M., Simulations of Heterogeneous Propellant Combustion: Effect of Particle Orientation and Shape, Proc. Combus. Inst., vol. 35, no. 2, pp. 2447-2454,2015.

  37. Prevost, M., Godon, J.C., and Innegraeve, O., Thrust Oscillations in Reduced Scale Solid Rocket Motors. Part I: Experimental Investigations, in 41st AIAA/ASME/SAE/ASEE Joint Propuls. Conf. Exhibit, AIAA Paper 2005-4003,2005.

  38. Salita, M., Modern SRM Ignition Transient Modeling. I-Introduction and Physical Models, in 37th Joint Propuls. Conf. Exhibit, AIAA Paper 2001-3443,2001.

  39. Torquato, S., Random Heterogeneous Materials: Microstructure and Macroscopic Properties, New York, NY: Springer-Verlag, 2002.

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