Numerical study of ignition and inter-sector flame propagation in gas turbine
For safety reasons, in-flight relight of the engine must be guaranteed over a wide range of operating conditions but the increasing stringency of pollutant emission constraints requires the development of new aero-engine combustor whose design might be detrimental to the ignition capability. To impr...
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| Format: | Others |
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2015
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| Online Access: | http://oatao.univ-toulouse.fr/15655/2/Esclapez_1.pdf http://oatao.univ-toulouse.fr/15655/3/Esclapez_2.pdf http://oatao.univ-toulouse.fr/15655/7/Esclapez_3.pdf |