For studying the structures of opposed mixing flow at the outlet of radial centripetal turbine
large eddy simulation was used to simulate the convective mixing flow of the circumferential intake. Flow structures in different modes were extracted and analyzed by the proper orthogonal decomposition (POD) method. The results showed that there existed stagnation zone near the bottom center and a recirculation zone near both sides of the wall
and the flow was approximately symmetrical at the horizontal cross section. The instability of the vortex structure was strengthened due to the effect of the shear force along the streamwise direction. Furthermore
the upstream three-dimensional vortex ring structure was stretched and expanded
breaking into a complex vortex braid or hairpin vortex structure
which enhanced the mixing
and also the momentum and energy exchanged between the fluids. The POD results showed that the first mode had the highest energy weight
indicating that most of the energy in the pulsating field was concentrated in this mode
and the flow structure in this mode acted as the main flow structure.
Large eddy simulation of cryogenic jet under supercritical pressure based on OpenFOAM
Analysis of n⁃dodecane spray jet by proper orthogonal decomposition
Large eddy simulation on the staggered tube bundle of the compact precooler
引用格式:王庆宇,刘琪麟,赖焕新.高亚声速喷流近场的流-声关联[J].航空动力学报,2020,35(12):2532-2542.WANG Qingyu,LIU Qilin,LAI Huanxin.Flow-acoustics correlations in near-fields of high subsonic jet[J].Journal of Aerospace Power,2020,35(12):2532-2542.Flow-acoustics correlations in near-fields of high subsonic jet
Large eddy simulation of low swirl premixed flame stabilization mechanism
Related Author
Yuhang LI
Baoyuan WU
Yi WANG
Lixin ZHOU
Wenjin QIN
Lihui XU
Dengbiao LU
Hao LIU
Related Institution
National Key Laboratory of Science and Technology on Liquid Rocket Engines,Xi'an Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
Academy of Aerospace Propulsion Technology,China Aerospace Science and Technology Corporation
Beijing Aerospace Institute for Metrology and Measurement Technology, China Academy of Launch Vehicle Technology, China Aerospace Science and Technology Corporation
School of Mechanical Engineering, University of Shanghai for Science and Technology
Research Institute of Aero-engine,Beijing University of Aeronautics and Astronautics