作者: G. Staffelbach , L. Y. M. Gicquel , T. Poinsot
DOI: 10.1007/978-3-540-34234-2_23
关键词: State (computer science) 、 Aerospace engineering 、 Industrial gas 、 Combustion chamber 、 Combustion instability 、 Electronic engineering 、 Computer science 、 Combustor 、 Parallel algorithm 、 Acoustic response 、 Large eddy simulation
摘要: Recent advances in computer science and highly parallel algorithms make Large Eddy Simulation (LES) an efficient tool for the study of complex flows. The available resources allow today to tackle full geometries that can not be installed laboratory facilities. present paper demonstrates state art LES allows simulations combustion chambers with one, three or all burners results may differ considerably from one configuration other. Computational needs issues such are discussed. A single burner periodic sector a triple annular chamber gas turbine investigated assess impact periodicity simplification. Cold flow validate this approach while reacting underline differences results. acoustic response set-up is totally different both cases so geometry seem requirement instability studies.