Experimental study of stability of supersonic boundary layer on swept wing

被引：0
|
作者：
Semionov, N. V. [1 ]
Kosinov, A. D. [1 ]
Yermolaev, Yu. G. [2 ]
机构：
[1] Inst Theoret & Appl Mech, Inst Skaya 4-1, Novosibirsk 630090, Russia
[2] Khristianovitch Inst, Theoret & Appl Mech, Novosibirsk 630090, Russia
来源：
SEVENTH IUTAM SYMPOSIUM ON LAMINAR-TURBULENT TRANSITION | 2010年 / 18卷
关键词：
D O I：
10.1007/978-90-481-3723-7_61
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
The paper is devoted to an experimental study of laminar-turbulent transition and instability disturbances evolution in a three-dimensional supersonic boundary layer on swept wing with sharp leading edge. The detailed data of natural disturbances development are obtained for the first time Characteristic zones of disturbances evolution are determined. A position of instability region of secondary flow is experimentally defined Some features of disturbances evolution, characteristic only for a supersonic boundary layer are revealed It was shown experimentally that secondary cross-flow instability plays the main role in laminar-turbulent transition in 3-D supersonic boundary layers.
引用
收藏
页码：379 / +
页数：2
相关论文
共 50 条
  • [41] Effect of Small Angles of Attack on Laminar-Turbulent Transition in the Supersonic Boundary Layer on a Swept Wing with χ = 72°
    Yu. G. Ermolaev
    A. D. Kosinov
    V. L. Kocharin
    A. N. Semenov
    N. V. Semionov
    S. A. Shipul’
    A. A. Yatskikh
    Fluid Dynamics, 2022, 57 : 30 - 36
  • [42] Effect of Small Angles of Attack on Laminar-Turbulent Transition in the Supersonic Boundary Layer on a Swept Wing with χ=72°
    Ermolaev, Yu G.
    Kosinov, A. D.
    Kocharin, V. L.
    Semenov, A. N.
    Semionov, N., V
    Shipul', S. A.
    Yatskikh, A. A.
    FLUID DYNAMICS, 2022, 57 (01) : 30 - 36
  • [43] Instability of the attachment line boundary layer in a supersonic swept flow
    Fedorov, Alexander, V
    Egorov, Ivan, V
    JOURNAL OF FLUID MECHANICS, 2022, 933
  • [44] Receptivity to Thermal Noise of the Boundary Layer over a Swept Wing
    Luchini, Paolo
    AIAA JOURNAL, 2017, 55 (01) : 121 - 130
  • [45] Wave forerunners of streamwise structures in a swept wing boundary layer
    V. N. Gorev
    M. M. Katasonov
    V. V. Kozlov
    Fluid Dynamics, 2007, 42 : 732 - 739
  • [46] Instability of a three-dimensional boundary layer on a swept wing
    V. Ya. Levchenko
    V. A. Scherbakov
    Journal of Applied Mechanics and Technical Physics, 1997, 38 (3) : 357 - 363
  • [47] Wave Forerunners of Streamwise Structures in a Swept Wing Boundary Layer
    Gorev, V. N.
    Katasonov, M. M.
    Kozlov, V. V.
    FLUID DYNAMICS, 2007, 42 (05) : 732 - 739
  • [48] Transition due to isolated roughness in a swept wing boundary layer
    Zoppini, Giulia
    Ragni, Daniele
    Kotsonis, Marios
    PHYSICS OF FLUIDS, 2022, 34 (08)
  • [49] Receptivity of the swept wing boundary layer to a steady flow inhomogeneity
    Ustinov M.V.
    Fluid Dynamics, 2001, 36 (3) : 437 - 447
  • [50] MEASUREMENTS IN THE TURBULENT BOUNDARY-LAYER ON AN INFINITE SWEPT WING
    BRADSHAW, P
    PONTIKOS, NS
    JOURNAL OF FLUID MECHANICS, 1985, 159 (OCT) : 105 - 130
12345