Direct numerical simulation of separation bubble in shock wave turbulent boundary layer interaction

被引:0
|
作者
Tong, Fulin [1 ,2 ,3 ]
Dong, Siwei [1 ,3 ]
Duan, Junyi [2 ,4 ]
Li, Xinjiang [2 ,4 ]
机构
[1] State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang,621000, China
[2] State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing,100190, China
[3] Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang,621000, China
[4] School of Engineering Science, University of Chinese Academy of Sciences, Beijing,100049, China
基金
中国国家自然科学基金;
关键词
Aspect ratio - Boundary layer flow - Boundary layers - Flow separation - Principal component analysis - Probability distributions - Separation - Shock waves;
D O I
10.7527/S1000-6893.2021.25437
中图分类号
学科分类号
摘要
Characteristics of separation bubbles in the interaction of a supersonic turbulent boundary layer at Mach number 2.25 with an impinging shock wave of 33.2° are investigated by means of Direct Numerical Simulation (DNS). After verifying the reliability of the numerical results, fundamental mechanisms associated with separation bubbles, including unsteadiness, separation micro-clusters geometries features and coherent structures, at three different spanwise locations are quantitatively compared to analyze the influence of the three-dimensionality in the spanwise direction. It is found that the separation bubble is highly three-dimensional, with the streamwise extent significantly larger than the wall-normal height and spanwise width. In the spanwise direction, the bubble height is generally large in the middle and small on both sides, exhibiting a single flat peak behavior. The pre-multiplied power spectrum density of the fluctuating separation bubble area suggests that the separation bubble unsteadiness is characterized by large-scale low-frequency contraction and dilation, which is less affected by the spanwise three-dimensionality. The bubbles on both sides lag slightly behind that in the middle. Conditional analysis based on Empirical Mode Decomposition (EMD) is performed to analyze the influence of the bubble dilation and contraction on geometries features of the separation micro-clusters. The statistical results indicate no essential changes in both motions, where the probability peak of the aspect ratio appears around 0.1, and the area and the normal height of the micro-clusters approximately satisfy the quadratic distribution. In addition, the Proper Orthogonal Decomposition (POD) analysis of the fluctuating streamwise velocity indicates that the unsteady motion of the separation bubble is strongly related to the low-order modes, whereas the contribution from the high-order modes is rather small. With the first ten low-order modes, the low-frequency dilation and contraction process of separation bubbles is accurately reconstructed. © 2022 AAAS Press of Chinese Society of Aeronautics and Astronautics. All rights reserved.
引用
收藏
相关论文
共 50 条
  • [1] Direct numerical simulation of conical shock wave-turbulent boundary layer interaction
    Zuo, Feng-Yuan
    Memmolo, Antonio
    Huang, Guo-ping
    Pirozzoli, Sergio
    [J]. JOURNAL OF FLUID MECHANICS, 2019, 877 : 167 - 195
  • [2] Direct numerical simulation of high enthalpy shock wave/turbulent boundary layer interaction
    Liu, Xiaodong
    Liu, Pengxin
    Li, Chen
    Sun, Dong
    Yuan, Xianxu
    [J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2023, 44 (13):
  • [3] The scaling of separation bubble in the conical shock wave/turbulent boundary layer interaction
    Zuo, Feng-Yuan
    [J]. ACTA ASTRONAUTICA, 2021, 186 : 418 - 425
  • [4] Direct Numerical Simulation Database for Impinging Shock Wave/Turbulent Boundary-Layer Interaction
    Pirozzoli, Sergio
    Bernardini, Matteo
    [J]. AIAA JOURNAL, 2011, 49 (06) : 1307 - 1312
  • [5] Direct Numerical Simulation of a Reflected-Shock-Wave/Turbulent-Boundary-Layer Interaction
    Priebe, S.
    Wu, A.
    Martin, M. P.
    [J]. AIAA JOURNAL, 2009, 47 (05) : 1173 - 1185
  • [6] Direct numerical simulation of impinging shock wave/turbulent boundary layer interaction at M=2.25
    Pirozzoli, Sergio
    Grasso, Francesco
    [J]. PHYSICS OF FLUIDS, 2006, 18 (06)
  • [7] NUMERICAL SIMULATION OF CROSSING SHOCK WAVE/TURBULENT BOUNDARY LAYER INTERACTION
    Kong Weixuan
    Zeng Peng
    Yan Chao
    Zhao Rui
    [J]. ELECTRICAL POWER & ENERGY SYSTEMS, PTS 1 AND 2, 2012, 516-517 : 954 - 959
  • [8] Direct numerical simulation of turbulence amplification in a strong shock-wave/turbulent boundary layer interaction
    Kang, Yujoo
    Lee, Sang
    [J]. PHYSICS OF FLUIDS, 2024, 36 (01)
  • [9] Wall temperature effects on shock wave/turbulent boundary layer interaction via direct numerical simulation
    Zhu, Ke
    Jiang, Lu-Xin
    Liu, Wei-Dong
    Sun, Ming-Bo
    Wang, Qian-Cheng
    Hu, Zhi-Wei
    [J]. ACTA ASTRONAUTICA, 2021, 178 : 499 - 510
  • [10] Modal Analysis of Separation Bubble Unsteadiness in Conical Shock Wave/Turbulent Boundary Layer Interaction
    Zuo, Feng-Yuan
    Yu, Ming
    Pirozzoli, Sergio
    [J]. AIAA JOURNAL, 2022, 60 (09) : 5123 - 5135