@article{1259dc637d8a4320a8d6e4e1fbc56ea4,
title = "Galloping and spinning modes of subsonic detonation",
abstract = "A reduced model for a pressure-driven subsonic combustion wave spreading through an inert porous medium (subsonic detonation) is derived. It is shown that the associated planar travelling wave solution may lose its stability assuming a galloping or spinning structure as occurs in supersonic free-space detonation. The problem of subsonic detonation is found to be dynamically akin to the problem of gasless combustion known for its rich pattern-forming dynamics.",
author = "I. Brailovsky and M. Frankel and G. Sivashinsky",
note = "Funding Information: The work of MF was supported by the NSF grant no DMS-9623006. The work of IB and GS was supported by the DOE grant no DE-FG02-88ER13822, by the US– Israel BSF grant no 9800374, by the Israel Science Foundation under grant no 40-98, by the Israel Ministry of Science under grant no 9685-1-97, by the Belfer Foundation for Energy Research and by the European Community Programmes INTAS-906-1173 and TMR-ERB FMRX CT98 0201 and the Research Foundation of Tel Aviv University (grant no 784). The numerical simulations were performed at the Israel Inter-University Computer Center.",
year = "2000",
month = mar,
doi = "10.1088/1364-7830/4/1/303",
language = "אנגלית",
volume = "4",
pages = "47--60",
journal = "Combustion Theory and Modelling",
issn = "1364-7830",
publisher = "Taylor and Francis Ltd.",
number = "1",
}