Flow structures in transitional and turbulent boundary layers

被引:108
|
作者
Lee, Cunbiao [1 ]
Jiang, Xianyang [1 ]
机构
[1] Peking Univ, Coll Engn, Adv Aero Engine Collaborat Innovat Ctr, State Key Lab Turbulence & Complex Syst, 5 Yiheyuan Rd, Beijing 100871, Peoples R China
基金
中国国家自然科学基金;
关键词
DIRECT NUMERICAL-SIMULATION; SCALE 3-DIMENSIONAL STRUCTURES; LINEAR-STABILITY THEORY; FLAT-PLATE; SECONDARY INSTABILITY; WALL REGION; STREAMWISE VORTICES; HAIRPIN VORTICES; ENTROPY-LAYER; COHERENT STRUCTURES;
D O I
10.1063/1.5121810
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The basic problems of transition in both incompressible and compressible boundary layers are reviewed. Flow structures in low-speed transitional and developed turbulent boundary layers are presented, together with almost all of the physical mechanisms that have been proposed for their formation. Comparisons of different descriptions of the same flow structures are discussed as objectively as possible. The importance of basic structure such as solitonlike coherent structure is addressed. For compressible flows, the receptivity and instability of boundary layer are reviewed, including the effect of different parameters on the transition. Finally, the principle of aerodynamic heating of hypersonic boundary layer is presented. (C) 2019 Author(s).
引用
收藏
页数:40
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