均匀吸力平板上层流边界层的近似解

IF 1.4 4区 工程技术 Q2 ENGINEERING, AEROSPACE
S. J. Peerless, D. B. Spalding
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引用次数: 0

摘要

边界层问题可分为两类:(a)可以找到类似解的问题,即边界条件使得在不同截面上存在仅在比例因子上不同的类似剖面;(b)边界条件不影响相似性的,因此边界层的发展必须分阶段计算。后一类问题被称为“延拓问题”,由于涉及的工作量,很少得到数值解。求解连续问题的近似方法是已知的,使用卡门动量积分法(例如参考文献1)或变体。其中一些方法利用“相似”边界层计算的速度剖面。本文提出了一种新的近似方法,它使用“相似”轮廓,但避免使用动量积分。而不是表征边界层厚度的“动量厚度”,需要计算,但不是直接感兴趣的,墙壁剪切应力被使用;这种应力通常在任何情况下都必须计算,因此本方法相对简单。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
An Approximate Solution of the Laminar Boundary Layer on a Flat Plate with Uniform Suction
Boundary layer problems may be divided into two classes: (a) those for which similar solutions can be found, i.e. where the boundary conditions are such that similar profiles differing only in scale factor exist at different sections; and (b) those where the boundary conditions do not effect similarity, so that the development of the boundary layer must be calculated in stages. The latter class are known as “continuation problems,” and very few numerical solutions have been obtained because of the labour involved. Approximate methods of solving continuation problems are known, using the Karman momentum integral method (e.g. Ref. 1) or variants. Some of these methods make use of velocity profiles calculated for “similar” boundary layers. This note presents a new approximate method which uses “similar” profiles but avoids using the momentum integral. Instead of characterising the boundary layer thickness by the “momentum thickness,” which needs to be calculated yet is of less direct interest, the wall shear stress is used; this stress usually has to be calculated in any case and the present method is therefore comparatively simple.
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来源期刊
Aeronautical Journal
Aeronautical Journal 工程技术-工程:宇航
CiteScore
3.70
自引率
14.30%
发文量
86
审稿时长
6-12 weeks
期刊介绍: The Aeronautical Journal contains original papers on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are therefore solicited on all aspects of research, design and development, construction and operation of aircraft and space vehicles. Papers are also welcomed which review, comprehensively, the results of recent research developments in any of the above topics.
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