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Volumn 18, Issue 5, 2002, Pages 1086-1092

Nonlinear heterogeneous model of composite solid-propellant combustion

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; COMPOSITE MATERIALS; HEAT CONDUCTION; MATHEMATICAL MODELS;

EID: 0036747417     PISSN: 07484658     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.6038     Document Type: Article
Times cited : (26)

References (13)
  • 1
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    • (1970) AIAA Journal , vol.8 , Issue.12 , pp. 2200-2207
    • Beckstead, M.1    Derr, R.2    Price, C.3
  • 2
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    • Examination of chemical approaches to stabilizing composite-propellant combustion
    • King, M., "Examination of Chemical Approaches to Stabilizing Composite-Propellant Combustion," Journal of Propulsion and Power, Vol. 12, No. 3, 1996, pp. 554-563.
    • (1996) Journal of Propulsion and Power , vol.12 , Issue.3 , pp. 554-563
    • King, M.1
  • 3
    • 0019589575 scopus 로고
    • Response function theories the account for size distribution effects: A review
    • Cohen, N., "Response Function Theories the Account for Size Distribution Effects: A Review," AIAA Journal, Vol. 19, No. 7, 1981, pp. 907-912.
    • (1981) AIAA Journal , vol.19 , Issue.7 , pp. 907-912
    • Cohen, N.1
  • 4
    • 0010871662 scopus 로고
    • Numerical computations of solid-propellant nonsteady burning in open or confined volumes
    • edited by L. De Luca, E. Price, and M. Summerfield; Progress in Astronautics and Aeronautics, AIAA, Washington, DC
    • Galfetti, L., Riva, G., and Bruno, C., "Numerical Computations of Solid-Propellant Nonsteady Burning in Open or Confined Volumes," Nonsteady Burning and Combustion Stability of Solid Propellants, edited by L. De Luca, E. Price, and M. Summerfield, Vol. 143, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1992, pp. 643-687.
    • (1992) Nonsteady Burning and Combustion Stability of Solid Propellants , vol.143 , pp. 643-687
    • Galfetti, L.1    Riva, G.2    Bruno, C.3
  • 6
    • 0018998686 scopus 로고
    • Review of composite propellant burn rate modeling
    • Cohen, N., "Review of Composite Propellant Burn Rate Modeling," AIAA Journal, Vol. 18, No. 3, 1980, pp. 277-293.
    • (1980) AIAA Journal , vol.18 , Issue.3 , pp. 277-293
    • Cohen, N.1
  • 7
    • 0029380404 scopus 로고
    • Quasi-steady combustion modeling of homogeneous solid propellants
    • Brewster, Q., and Son, S., "Quasi-Steady Combustion Modeling of Homogeneous Solid Propellants," Combustion and Flame, Vol. 103, No. 1/2, 1995, pp. 11-26.
    • (1995) Combustion and Flame , vol.103 , Issue.1-2 , pp. 11-26
    • Brewster, Q.1    Son, S.2
  • 8
    • 85007219760 scopus 로고
    • A model of solid propellant combustion including surface heterogeneity and heat generation
    • Hermance, C. E., "A Model of Solid Propellant Combustion Including Surface Heterogeneity and Heat Generation," AIAA Journal, Vol. 4, No. 9, 1966, pp. 1629-1637.
    • (1966) AIAA Journal , vol.4 , Issue.9 , pp. 1629-1637
    • Hermance, C.E.1
  • 9
    • 0018506637 scopus 로고
    • Oxidizer size distribution effects on propellant combustion
    • Renie, J., Condon, J., and Osborn, J., "Oxidizer Size Distribution Effects on Propellant Combustion," AIAA Journal, Vol. 17, No. 8, 1979, pp. 877-883.
    • (1979) AIAA Journal , vol.17 , Issue.8 , pp. 877-883
    • Renie, J.1    Condon, J.2    Osborn, J.3
  • 10
    • 4244185228 scopus 로고    scopus 로고
    • Modeling of aluminized solid propellants
    • ONERA, Technical Report RT 37/7128 EN, Palaiseau, France
    • Bellec, R., Duterque, J., and Lengellé, G., "Modeling of Aluminized Solid Propellants," ONERA, Technical Report RT 37/7128 EN, Palaiseau, France, 1996.
    • (1996)
    • Bellec, R.1    Duterque, J.2    Lengellé, G.3
  • 11
    • 0026330005 scopus 로고
    • Chemistry and kinetics of hydroxyl-terminated polybutadiene (HTPB) and diisocyanate-HTPB polymers during slow decomposition and combustion-like conditions
    • Chen, J., and Brill, T., "Chemistry and Kinetics of Hydroxyl-terminated Polybutadiene (HTPB) and Diisocyanate-HTPB Polymers During Slow Decomposition and Combustion-like Conditions," Combustion and Flame, Vol. 87, 1991, pp. 217-232.
    • (1991) Combustion and Flame , vol.87 , pp. 217-232
    • Chen, J.1    Brill, T.2
  • 12
    • 0010796455 scopus 로고    scopus 로고
    • A kinetic model for the premixed combustion of a fine AP/HTPB composite propellant
    • AIAA Paper 98-0447, Jan
    • Jeppson, M., Beckstead, M., and Jing, Q., "A Kinetic Model for the Premixed Combustion of a Fine AP/HTPB Composite Propellant," AIAA Paper 98-0447, Jan. 1998.
    • (1998)
    • Jeppson, M.1    Beckstead, M.2    Jing, Q.3
  • 13
    • 4243519186 scopus 로고    scopus 로고
    • Temperature sensitivity measurements of solid rocket propellants
    • M.S.E. Thesis, Dept. of Mechanical and Aerospace Engineering, Univ. of Alabama in Huntsville, AL, Spring, Feb
    • Rochford, E., "Temperature Sensitivity Measurements of Solid Rocket Propellants," M.S.E. Thesis, Dept. of Mechanical and Aerospace Engineering, Univ. of Alabama in Huntsville, AL, Spring, Feb. 1999.
    • (1999)
    • Rochford, E.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.