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Analysis of the dominant frequency in a subsonic compressor stator at near stall condition
  • ISSN号:1001-246X
  • 期刊名称:《计算物理》
  • 时间:0
  • 分类:O357.41[理学—流体力学;理学—力学] O354.4[理学—流体力学;理学—力学]
  • 作者机构:[1]Department of Mechanism, Tianjin University, Tianjin 300072, China, [2]School of Aerospace Engineering, Tsinghua University, Beijing 100181, China
  • 相关基金:Project supported by the National Natural Science Foundation of China (Nos. 11272183, 11572176, 11402167, 11202147, and 11332007) and the National Program on Key Basic Research Project of China (No. 2014CB744801),Acknowledgements Thanks to Jie REN in Tsinghua University for supplying the Gothler flow, Xuezhi LU in Tianjin University for supplying the crossflow vortices, and Runjie SONG in Tianjin University for supplying the evolution on the wave-packet disturbance in the hypersonic boundary layer.
作者: Ke Shi Song Fu[1]
中文摘要:

It is widely accepted that a robust and efficient method to compute the linear spatial amplified rate ought to be developed in three-dimensional(3D) boundary layers to predict the transition with the e~N method,especially when the boundary layer varies significantly in the spanwise direction.The 3D-linear parabolized stability equation(3DLPSE) approach,a 3D extension of the two-dimensional LPSE(2D-LPSE),is developed with a plane-marching procedure for investigating the instability of a 3D boundary layer with a significant spanwise variation.The method is suitable for a full Mach number region,and is validated by computing the unstable modes in 2D and 3D boundary layers,in both global and local instability problems.The predictions are in better agreement with the ones of the direct numerical simulation(DNS) rather than a 2D-eigenvalue problem(EVP) procedure.These results suggest that the plane-marching 3D-LPSE approach is a robust,efficient,and accurate choice for the local and global instability analysis in 2D and 3D boundary layers for all free-stream Mach numbers.

英文摘要:

It is widely accepted that a robust and efficient method to compute the linear spatial amplified rate ought to be developed in three-dimensional (3D) boundary layers to predict the transition with the e^N method, especially when the boundary layer varies significantly in the spanwise direction. The 3D-linear parabolized stability equation (3D- LPSE) approach, a 3D extension of the two-dimensional LPSE (2D-LPSE), is developed with a plane-marching procedure for investigating the instability of a 3D boundary layer with a significant spanwise variation. The method is suitable for a full Mach number region, and is validated by computing the unstable modes in 2D and 3D boundary layers, in both global and local instability problems. The predictions are in better agreement with the ones of the direct numerical simulation (DNS) rather than a 2D-eigenvalue problem (EVP) procedure. These results suggest that the plane-marching 3D-LPSE approach is a robust, efficient, and accurate choice for the local and global instability analysis in 2D and 3D boundary layers for all free-stream Mach numbers.

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期刊信息
  • 《计算物理》
  • 中国科技核心期刊
  • 主管单位:中国科学技术协会
  • 主办单位:中国核学会
  • 主编:朱少平
  • 地址:北京海淀区丰豪东路2号北京应用物理与计算数学研究所
  • 邮编:100094
  • 邮箱:jswl@iapcm.ac.cn
  • 电话:010-59872547 59872545 59872547
  • 国际标准刊号:ISSN:1001-246X
  • 国内统一刊号:ISSN:11-2011/O4
  • 邮发代号:2-477
  • 获奖情况:
  • 1992年获“全优期刊”奖,《CAJ-CD规范》执行优秀奖
  • 国内外数据库收录:
  • 荷兰文摘与引文数据库,日本日本科学技术振兴机构数据库,中国中国科技核心期刊,中国北大核心期刊(2004版),中国北大核心期刊(2008版),中国北大核心期刊(2011版),中国北大核心期刊(2014版),中国北大核心期刊(2000版)
  • 被引量:4426