TRANSVERSE CURVATURE EFFECT ON INCOMPRESSIBLE LAMINAR BOUNDARY LAYER FOR LONGITUDINAL FLOW OVER A CYLINDER

被引：24

作者：

JAFFE, NA

OKAMURA, TT

机构：

[1] McDonnell Douglas Corp., Douglas Aircraft Co., Long Beach, Calif.

来源：

ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND PHYSIK | 1968年 / 19卷 / 04期

关键词：

D O I：

10.1007/BF01594964

中图分类号：

O29 [应用数学];

学科分类号：

070104 ;

摘要：

A solution to the partial differential equations governing incompressible laminar flow in the axial direction over a circular cylinder is presented. A method is employed which reduces the partial differential equations to a set of ordinary differential equations which are then solved consecutively. The solution is initiated at a leading edge and proceeds far downstream. Velocity profiles and values for the coefficient of skin friction, displacement thickness and momentum thickness are obtained. The results are compared to previously obtained solutions valid near the leading edge and asymptotic solutions valid far downstream. © 1968 Birkhäuser Verlag.

引用

页码：564 / &

共 10 条

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