The large-eddy simulation was carried out to research convective heat transfer in the staggered tube bundle of the compact precooler. Besides
the dynamic mode decomposition (DMD) method was used to analyze the coherent structure and statistical characteristic of heat transfer of cross-row tube bundles. Results showed that within the simulated operating range (Re≤6 000)
the flow structure of the front tube bundle exhibited regular shear layer movement and wake vortex shedding. The flow structure of the rear tube bundle was an irregular small-scale vortex structure
and the disorderly flow field of the rear tube bundle was presented. The instantaneous Nusselt number on the surface of the front rows had a relatively fixed wave frequency
while the instantaneous Nu on the back rows had no fixed wave frequency because of the irregular impact of the falling vortex of the front rows. Under the condition of Re=2 600
the entropy production in the bundle mainly came from heat transfer rather than dissipation. The main flow structure contributed to the dissipative entropy production and heat transfer entropy production in the location of the boundary layer and free shear layer on the tube wall. It contributed greatly to the entropy production in the front row tubes
but less to the entropy production in the back row tubes.
Coherent structures of cascade under different attack angles with DMD method
Large eddy simulation of cryogenic jet under supercritical pressure based on OpenFOAM
Analysis of n⁃dodecane spray jet by proper orthogonal decomposition
Study on opposed mixing flow in circumferential intake
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
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Related Institution
南京航空航天大学 能源与动力学院 江苏省航空动力系统重点实验室
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