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
  • [41] Roughness-Induced Transition in a Supersonic Boundary Layer
    Balakumar, P.
    Kegerise, Michael
    AIAA JOURNAL, 2016, 54 (08) : 2322 - 2337
  • [42] Role of Transient Growth in Roughness-Induced Transition
    Reshotko, Eli
    Tumin, Anatoli
    1600, American Inst. Aeronautics and Astronautics Inc. (42):
  • [43] Roughness-Induced Transition of Hypervelocity Boundary Layers
    Wise, Dylan J.
    Smart, Michael K.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2014, 51 (03) : 847 - 854
  • [44] Triadic Resonance Analysis of Distributed Roughness Effects on Crossflow Instability in Swept-Wing Boundary Layers
    Xu, Jiakuan
    He, Jiyang
    Wu, Xuesong
    IUTAM LAMINAR-TURBULENT TRANSITION, 2022, 38 : 825 - 836
  • [45] Applications of EPSE method for predicting crossflow instability in swept-wing boundary layers
    Lu, Xuezhi
    Luo, Jisheng
    APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2017, 38 (07) : 981 - 996
  • [46] Transition due to isolated roughness in a swept wing boundary layer
    Zoppini, Giulia
    Ragni, Daniele
    Kotsonis, Marios
    PHYSICS OF FLUIDS, 2022, 34 (08)
  • [47] Applications of EPSE method for predicting crossflow instability in swept-wing boundary layers
    Xuezhi LU
    Jisheng LUO
    Applied Mathematics and Mechanics(English Edition), 2017, 38 (07) : 981 - 996
  • [48] Delay of Laminar-Turbulent Transition on Swept-Wing with Help of Sweeping Surface Relief
    Ivanov, A. V.
    Mischenko, D. A.
    HIGH ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2019), 2019, 2125
  • [49] Discrete-Roughness-Element-Enhanced Swept-Wing Natural Laminar Flow at High Reynolds Numbers
    Malik, Mujeeb
    Liao, Wei
    Li, Fei
    Choudhari, Meelan
    AIAA JOURNAL, 2015, 53 (08) : 2321 - 2334
  • [50] Applications of EPSE method for predicting crossflow instability in swept-wing boundary layers
    Xuezhi Lu
    Jisheng Luo
    Applied Mathematics and Mechanics, 2017, 38 : 981 - 996
12345