Comparison of amplitude method of roughness-induced swept-wing transition prediction with experiment

被引：7
|
作者：
Ustinov, M. V. [1 ]
Kachanov, Y. S. [2 ]
机构：
[1] Cent Aerohydrodynam Inst TsAGI, 1 Zhukovsky Str, Zhukovskii 140180, Russia
[2] Khristianovich Inst Theoret & Appl Mech, Novosibirsk 630090, Russia
来源：
PHYSICS OF FLUIDS | 2021年 / 33卷 / 09期
基金：
俄罗斯科学基金会;
关键词：
3-DIMENSIONAL BOUNDARY-LAYER; CROSS-FLOW VORTICES; SECONDARY INSTABILITY; STABILITY; RECEPTIVITY;
D O I：
10.1063/5.0057853
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
An amplitude method of laminar-turbulent transition prediction in the boundary layer on a swept wing has been developed and tested. The method computes the amplitudes and spectra of steady cross-flow instability modes generated by surface roughness. The transition criterion is based on the crucial, threshold values of maximal or local amplitudes of these perturbations found from experiments. Statistical methods describing the intermittency in the transition zone based on this criterion are proposed.
引用
收藏
页数：16
相关论文
共 50 条
  • [1] Description and Prediction of Roughness-Induced Transition in Swept-Wing Boundary Layers
    Boiko, Andrey V.
    Borodulin, Vladimir I.
    Ivanov, Andrey V.
    Kirilovskiy, Stanislav V.
    Mischenko, Dmitry A.
    Poplavskaya, Tatiana V.
    AIAA JOURNAL, 2025,
  • [2] Amplitude method of prediction of laminar-turbulent transition on a swept-wing
    M. V. Ustinov
    Fluid Dynamics, 2017, 52 : 71 - 87
  • [3] Amplitude method of prediction of laminar-turbulent transition on a swept-wing
    Ustinov, M. V.
    FLUID DYNAMICS, 2017, 52 (01) : 71 - 87
  • [4] Roughness-induced receptivity to crossflow vortices on a swept wing
    Ng, LL
    Crouch, JD
    PHYSICS OF FLUIDS, 1999, 11 (02) : 432 - 438
  • [5] Progress in Development of Amplitude Method of Transition Prediction on Swept Wing
    Ustinov, Maksim, V
    IUTAM LAMINAR-TURBULENT TRANSITION, 2022, 38 : 71 - 83
  • [6] Effect of isolated micron-sized roughness on transition in swept-wing flows
    Radeztsky, RH
    Reibert, MS
    Saric, WS
    AIAA JOURNAL, 1999, 37 (11) : 1370 - 1377
  • [7] Roughness receptivity in swept-wing boundary layers - experiments
    Carpenter, Andrew L.
    Saric, William S.
    Reed, Helen L.
    INTERNATIONAL JOURNAL OF ENGINEERING SYSTEMS MODELLING AND SIMULATION, 2010, 2 (1-2) : 128 - 138
  • [8] Roughness receptivity in swept-wing boundary layers - computations
    Rhodes, Richard G.
    Reed, Helen L.
    Saric, William S.
    Carpenter, Andrew L.
    Neale, Tyler P.
    INTERNATIONAL JOURNAL OF ENGINEERING SYSTEMS MODELLING AND SIMULATION, 2010, 2 (1-2) : 139 - 148
  • [9] Infinite swept-wing Navier-Stokes computations with eN transition prediction
    Stock, HW
    AIAA JOURNAL, 2005, 43 (06) : 1221 - 1229
  • [10] Infinite swept-wing Navier-Stokes computations with eN transition prediction
    Stock, H.W., 1600, American Inst. Aeronautics and Astronautics Inc. (43):
12345