摘要 : In order to evaluate the direct and indirect contributions to the total combustion noise emission, a combustion chamber consisting of a swirl burner and an exit nozzle of Laval-shape, representing a gas turbine combustor, is inves... 展开
作者 | Flemming F Olbricht C Wegner B Sadiki A Janicka J Bake F Michel U Lehmann B Rohle I |
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作者单位 | |
期刊名称 | 《Flow, turbulence and combustion》 |
总页数 | 25 |
语种/中图分类号 | 英语 / O3 |
关键词 | gas turbine combustor large eddy simulation noise sources length scales precessing vortex core LARGE-EDDY SIMULATION DIFFUSION FLAME TURBULENT COMBUSTION VORTEX CORE INSTABILITY SWIRL |
馆藏号 | N2008EPST0000782 |