Evolution of nonlinear processes in a hypersonic boundary layer on a sharp cone

被引:50
|
作者
Bountin, D. [1 ]
Shiplyuk, A. [1 ]
Maslov, A. [1 ]
机构
[1] Russian Acad Sci, Khristianovich Inst Theoret & Appl Mech, Novosibirsk 630090, Russia
基金
俄罗斯基础研究基金会;
关键词
D O I
10.1017/S0022112008003030
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Nonlinear processes in a hypersonic boundary layer on a sharp cone are considered using, the bicoherence method. The experiments are performed for a Mach number M-x = 5.95 with introduction of artificial wave packets at the frequency of the second mode. It is shown that the basic mechanism of nonlinear interaction at the location of the maximum r.m.s. voltage fluctuation is the subharmonic resonance; all nonlinear interactions in the maximum r.m.s. voltage fluctuation layer are related to the second mode of disturbances; nonlinear processes above and below that layer are much more intense than those in it. The effect of artificial disturbances on nonlinear interaction's in the boundary layer is shown to be insignificant.
引用
收藏
页码:427 / 442
页数:16
相关论文
共 50 条
  • [21] Hypersonic boundary-layer transition on a flared cone
    Chuan-Hong Zhang
    Qing Tang
    Cun-Biao Lee
    Acta Mechanica Sinica, 2013, 29 : 48 - 54
  • [22] Hypersonic boundary-layer transition on a flared cone
    Zhang, Chuan-Hong
    Tang, Qing
    Lee, Cun-Biao
    ACTA MECHANICA SINICA, 2013, 29 (01) : 48 - 53
  • [23] Hypersonic boundary-layer transition on a flared cone
    Chuan-Hong Zhang
    Qing Tang
    Cun-Biao Lee
    Acta Mechanica Sinica, 2013, 29 (01) : 48 - 53
  • [24] Experimental Investigation of the Effect of a Passive Porous Coating on a Hypersonic Boundary Layer Stability on a Sharp Cone at an Angle of Attack
    Lukashevich, S. V.
    Morozov, S. O.
    Shiplyuk, A. N.
    XV ALL-RUSSIAN SEMINAR DYNAMICS OF MULTIPHASE MEDIA, 2018, 1939
  • [25] Interaction of second-mode instability and distributed roughness elements in the hypersonic boundary layer over a sharp cone
    Li, Xueliang
    Gui, Yuteng
    Li, Chuangchuang
    Su, Wei
    Wu, Jie
    AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 155
  • [26] EXPANSION OF A HYPERSONIC TURBULENT BOUNDARY-LAYER AT A SHARP CORNER
    BLOY, AW
    JOURNAL OF FLUID MECHANICS, 1975, 67 (FEB25) : 647 - &
  • [27] Evolution of the second mode in a hypersonic boundary layer
    Zhang, Chuanhong
    PHYSICS OF FLUIDS, 2020, 32 (12)
  • [28] Nonlinear wave processes in a hypersonic shock layer
    Maslov, A. A.
    Poplavskaya, T. V.
    Tsyryul'nikov, I. S.
    FLUID DYNAMICS, 2010, 45 (04) : 552 - 558
  • [29] Nonlinear wave processes in a hypersonic shock layer
    A. A. Maslov
    T. V. Poplavskaya
    I. S. Tsyryul’nikov
    Fluid Dynamics, 2010, 45 : 552 - 558
  • [30] Experiment of Hypersonic Boundary Layer Transition on a Cone with Axisymmetric Step
    Xu X.-W.
    Yi S.-H.
    Zhang F.
    Xiong H.-X.
    Shi Y.
    Yuhang Xuebao/Journal of Astronautics, 2019, 40 (08): : 908 - 917