Two-phase unsteady flow in solid rocket motors
Aluminized propellants are frequently used in solid rocket motors to increase specific impulse. Unlike the other ingredients, aluminum particles can burn in a significant portion of the chamber and produce a condensed phase that is carried out into the flowfield. Thereby, aluminum particles can affe...
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| Published in | Aerospace science and technology Vol. 6; no. 6; pp. 413 - 422 |
|---|---|
| Main Author | |
| Format | Journal Article |
| Language | English |
| Published |
Paris
Elsevier SAS
01.10.2002
Elsevier |
| Subjects | |
| Online Access | Get full text |
| ISSN | 1270-9638 1626-3219 |
| DOI | 10.1016/S1270-9638(02)01182-3 |
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| Abstract | Aluminized propellants are frequently used in solid rocket motors to increase specific impulse. Unlike the other ingredients, aluminum particles can burn in a significant portion of the chamber and produce a condensed phase that is carried out into the flowfield. Thereby, aluminum particles can affect appreciably combustion instabilities by acting as driving or, on the contrary, as damping mechanisms. Therefore, a reliable stability prediction must include the description of the reactive two-phase flow in the motor. Studies realized on this subject in the ASSM program are reviewed.
Les propergols aluminisés sont fréquemment utilisés dans les moteurs à propergol solide pour augmenter l'impulsion spécifique. Contrairement aux autres ingrédients du propergol, les particules d'aluminium peuvent brûler dans une portion significative de la chambre et produire une phase condensée qui est transportée dans l'écoulement. De ce fait, les particules d'aluminium peuvent modifier sensiblement les instabilités de combustion en les amplifiant ou, au contraire, en les réduisant. C'est pourquoi, une prédiction fiable de la stabilité doit inclure la description de l'écoulement diphasique dans le moteur. Les études réalisées sur ce sujet dans le programme ASSM sont présentées. |
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| AbstractList | Aluminized propellants are frequently used in solid rocket motors to increase specific impulse. Unlike the other ingredients, aluminum particles can burn in a significant portion of the chamber and produce a condensed phase that is carried out into the flowfield. Thereby, aluminum particles can affect appreciably combustion instabilities by acting as driving or, on the contrary, as damping mechanisms. Therefore, a reliable stability prediction must include the description of the reactive two-phase flow in the motor. Studies realized on this subject in the ASSM program are reviewed.
Les propergols aluminisés sont fréquemment utilisés dans les moteurs à propergol solide pour augmenter l'impulsion spécifique. Contrairement aux autres ingrédients du propergol, les particules d'aluminium peuvent brûler dans une portion significative de la chambre et produire une phase condensée qui est transportée dans l'écoulement. De ce fait, les particules d'aluminium peuvent modifier sensiblement les instabilités de combustion en les amplifiant ou, au contraire, en les réduisant. C'est pourquoi, une prédiction fiable de la stabilité doit inclure la description de l'écoulement diphasique dans le moteur. Les études réalisées sur ce sujet dans le programme ASSM sont présentées. Aluminized propellants are frequently used in solid rocket motors to increase specific impulse. Unlike the other ingredients, aluminum particles can burn in a significant portion of the chamber and produce a condensed phase that is carried out into the flowfield. In this way, aluminum particles can appreciably affect combustion instabilities by acting as driving or, on the contrary, as damping mechanisms. Therefore, a reliable stability prediction must include the description of the reactive two-phase flow in the motor. Studies realized on this subject in the ASSM program are reviewed. (Author) |
| Author | Dupays, Joël |
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| Cites_doi | 10.1108/09615539710185604 10.2514/6.1996-761 10.2514/2.5924 10.2514/6.1996-3248 10.2514/3.49907 10.2514/6.1998-3824 10.1080/00102207308952359 10.1016/S0010-2180(99)00128-5 10.2514/3.23888 10.2514/3.23902 10.2514/2.5570 10.1121/1.1910073 10.2514/6.2000-818 10.2514/6.1980-1091 10.2514/6.1997-2859 10.2514/6.2001-3947 10.2514/6.1995-2733 |
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| Keywords | Solid rocket motor Instabilités de combustion Combustion de l'aluminium Two-phase flow Propulsion propergol solide Aluminum combustion Numerical simulation Écoulement diphasique Simulation numérique Combustion instabilities Combustion instability Two phase flow Heat engine Solid propellant Aluminium Unsteady flow Rocket |
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| References_xml | – reference: P. Villedieu, J. Hylkema, G. Lavergne, B. Platet, Y. Fabignon, M. Vardelle, J.F. Guéry, F. Godfroy, P. Le Helley, L. Jacques, Slag accumulation in solid-propellant rocket motors with a submerged nozzle, in: 2nd European Conference on Launcher Technology, Rome, Italy, November 21–24, 2000 – volume: 18 start-page: 222 year: 2002 end-page: 224 ident: BIB011 article-title: Propagation of acoustic waves in a two-phase vaporizing mixture publication-title: J. Propul. Power – volume: 185 start-page: 859 year: 2000 end-page: 883 ident: BIB014 article-title: Some aspects of two-phase flows in solid-propellant rocket motors publication-title: Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics – volume: 7 start-page: 722 year: 1997 end-page: 736 ident: BIB001 article-title: Analytical and numerical results on the attenuation and dispersion of an acoustic wave through a two-phase flow publication-title: Int. J. Num. Meth. 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| SubjectTerms | Aluminum combustion Applied sciences Combustion de l'aluminium Combustion instabilities Energy Energy. Thermal use of fuels Engines and turbines Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc Exact sciences and technology Instabilités de combustion Numerical simulation Propulsion propergol solide Simulation numérique Solid rocket motor Two-phase flow Écoulement diphasique |
| Title | Two-phase unsteady flow in solid rocket motors |
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