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Physical basis and mathematical model of the propagation of a flame over the surface of a solid propellant during ignition

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Combustion, Explosion and Shock Waves Aims and scope

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References

  1. S. De Soto and H. A. Friedman, AIAA J.,3, 3, 1965.

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  2. K. H. Parker, W. I. Most, and M. Summerfield, Astronautical acta,12, 4, 1966.

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  3. R. F. McAlevy, R. S. Magee, et al., AIAA J.,5, 2, 1967.

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Authors
  1. B. A. Raizberg
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Additional information

Fizika Goreniya i Vzryva, Vol. 4, No. 4, pp. 568–578, 1968

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Raizberg, B.A. Physical basis and mathematical model of the propagation of a flame over the surface of a solid propellant during ignition. Combust Explos Shock Waves 4, 330–335 (1968). https://doi.org/10.1007/BF00742575

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  • DOI: https://doi.org/10.1007/BF00742575

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