The law of the wake in the turbulent boundary layer

Author:

Coles Donald

Abstract

After an extensive survey of mean-velocity profile measurements in various two-dimensional incompressible turbulent boundary-layer flows, it is proposed to represent the profile by a linear combination of two universal functions. One is the well-known law of the wall. The other, called the law of the wake, is characterized by the profile at a point of separation or reattachment. These functions are considered to be established empirically, by a study of the mean-velocity profile, without reference to any hypothetical mechanism of turbulence. Using the resulting complete analytic representation for the mean-velocity field, the shearing-stress field for several flows is computed from the boundary-layer equations and compared with experimental data.The development of a turbulent boundary layer is ultimately interpreted in terms of an equivalent wake profile, which supposedly represents the large-eddy structure and is a consequence of the constraint provided by inertia. This equivalent wake profile is modified by the presence of a wall, at which a further constraint is provided by viscosity. The wall constraint, although it penetrates the entire boundary layer, is manifested chiefly in the sublayer flow and in the logarithmic profile near the wall.Finally, it is suggested that yawed or three-dimensional flows may be usefully represented by the same two universal functions, considered as vector rather than scalar quantities. If the wall component is defined to be in the direction of the surface shearing stress, then the wake component, at least in the few cases studied, is found to be very nearly parallel to the gradient of the pressure.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference29 articles.

1. Wieghardt, K. 1943 Über die Wandschubspannung in turbulenten Reibungsschichten bei veränderlichem Aussendruck,Z. W. B., K. W. I., Göttingen, U. & M. 6603. See also Wieghardt, K. & Tillmann, W., Zur turbulenten Reibungsschicht bei Druckanstieg, Z. W. B., K. W. I., Göttingen, U. & M. 6617, 1944; translated as On the turbulent friction layer for rising pressure, Nat. Adv. Comm. Aero., Wash., Tech. Mem. no. 1314, 1951.

2. Schubauer, G. & Klebanoff, P. 1950 Investigation of separation of the turbulent boundary layer,Nat. Adv. Comm. Aero., Wash., Tech. Note no. 2133.

3. Rotta, J. 1950 Über die Theorie der turbulenten Grenzschichten,Mitt. Max-Planck-Inst., Göttingen, No. 1; translated as On the theory of the turbulent boundary layer, Nat. Adv. Comm. Aero., Wash., Tech. Mem. no. 1344, 1953.

4. Coles, D. 1954 The problem of the turbulent boundary layer,Z. angew. Math. Phys.,5,181–203.

5. Sheppard, P. 1947 The aerodynamic drag of the earth's surface and the value of von Kármán's constant in the lower atmosphere,Proc. Roy. Soc. A,188,208–222.

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3