Growth of boundary-layer streaks due to free-stream turbulence

被引:8
作者
Ricco, Pierre [1 ]
Walsh, Edmond J. [2 ]
Brighenti, Flavio [3 ]
McEligot, Donald M. [4 ,5 ]
机构
[1] Univ Sheffield, Dept Mech Engn, Sheffield S1 3JD, S Yorkshire, England
[2] Univ Oxford, Dept Engn Sci, Oxford OX2 0ES, England
[3] Karlsruhe Inst Technol, Inst Tech Phys, Campus North, D-76344 Karlsruhe, Germany
[4] Univ Idaho, Dept Mech Engn, Idaho Falls, ID 83401 USA
[5] Univ Arizona, Dept Aerosp & Mech Engn, Tucson, AZ 85721 USA
基金
英国工程与自然科学研究理事会;
关键词
Boundary layers; Transition to turbulence; NONLINEAR INSTABILITIES; BYPASS TRANSITION; PRESSURE-GRADIENT; DISTURBANCES; UPSTREAM; FLOW; BREAKDOWN; VORTICES; SUBJECT; DECAY;
D O I
10.1016/j.ijheatfluidflow.2016.05.003
中图分类号
O414.1 [热力学];
学科分类号
摘要
The growth of laminar boundary-layer streaks caused by free-stream turbulence encountering a flat plate in zero-pressure-gradient conditions is investigated experimentally in a wind tunnel and numerically by solving the unsteady boundary-region equations. A comparative discussion amongst the most relevant theoretical frameworks, such as the Goldstein theory, the Taylor-Stewartson theory, the optimal-growth theory and the Orr-Sommerfeld theory, is first presented and parallels and complimentary aspects of the theories are pointed out to justify the use of the Goldstein theory in our study. The statistical prop erties of the positive and negative fluctuations of the laminar streaks are discussed, showing how the total time average of the boundary-layer fluctuations masks the true character of the disturbance flow and revealing that the maximum values and the root-mean-square of positive and negative fluctuations grow downstream at the same rate. The downstream growth rate of the low-frequency disturbances and the decay rate of the high-frequency disturbances are also computed for the first time. The numerical solutions of the unsteady boundary-region equations are compared successfully with the streak profiles measured in the wind tunnel and with direct numerical simulation results available in the literature. (C) 2016 Elsevier Inc. All rights reserved.
引用
收藏
页码:272 / 283
页数:12
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