Abstract
The transition to detonation in gases is a very complicated multifaceted process. Turbulent mixing, interaction of acoustic waves with underlying chemical reactions, formation of regularly spaced Mach stem structures—this is just a partial list of phenomena taking part in the transition from deflagration to a self-sustained detonation. (See the review article [7] for an experimentalist’s summary). In this paper through carefully documented numerical experiments we investigate one aspect of the transition process which is also related to the direct initiation of reacting shock waves.
Partially supported by research grants A.R.O. #DAAL03–86-K-003, and O.N.R. #N00014–85-K-0507
Partially supported by the National Science Foundation under grant DMS-8603506.
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References
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© 1988 Springer-Verlag New York Inc.
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Majda, A., Roytburd, V. (1988). Numerical Modeling of the Initiation of Reacting Shock Waves. In: Engquist, B., Majda, A., Luskin, M. (eds) Computational Fluid Dynamics and Reacting Gas Flows. The IMA Volumes in Mathematics and Its Applications, vol 12. Springer, New York, NY. https://doi.org/10.1007/978-1-4612-3882-9_11
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DOI: https://doi.org/10.1007/978-1-4612-3882-9_11
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