Skin-Friction and Surface-Pressure Structures in Near-Wall Flows

被引:28
|
作者
Liu, Tianshu [1 ]
机构
[1] Western Michigan Univ, Dept Mech & Aerosp Engn, Kalamazoo, MI 49008 USA
关键词
SEPARATION; SHOCK;
D O I
10.2514/1.J057216
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Skin-friction tau and surface-pressure p in a viscous flow constitute a pair of the intrinsically coupled physical quantities denoted by the notation (tau, p), which determines the near-wall flow structures. The exact (tau, p) relation derived from the Navier-Stokes (NS) equations provides a rational foundation for reconstruction of the (tau, p) structures in complex flows. Based on this coupling relation, a tau field can be obtained from the perturbed p field for the given boundary enstrophy flux field of a base flow as an inverse problem in the first-order approximation. Then, the corresponding near-wall velocity field is reconstructed by using the Taylor-series-expansion solution of the NS equations. Some elemental and complex (tau, p) structures in three-dimensional flow separations are reconstructed to demonstrate the applicability of the proposed method.
引用
收藏
页码:3887 / 3896
页数:10
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