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3-Dimensional Fluid Flow Analysis for Aerodynamic Response Characteristics of Rectangular Cylinder

矩形圆柱体气动响应特性的三维流体流动分析

基本信息

批准号：
09650533
负责人：
HIRANO Hirokazu
金额：
$ 1.66万
依托单位：
Chuo University
依托单位国家：
日本
项目类别：
Grant-in-Aid for Scientific Research (C)
财政年份：
1997
资助国家：
日本
起止时间：
1997 至 1999
项目状态：
已结题

项目摘要

It has become clear that 3-dimensional analysis is required in a certain Reynolds number range, when expressing, by numerical fluid flow analysis, the accurate aerodynamic characteristics and the state of flow around a rectangular sectioned member in which the separation shear layer separates at the front edge and reattaches to the rear surface of the member, as represented by a flat surfaced box-girder bridge. The main results are the following:(1) The 3-dimensional analysis facilitates qualitative understanding of the aerodynamic characteristics and the state of flow around a rectangular member indicated by the results of wind tunnel tests. Moreover, the separation shear layer which separated at the front edge reattaches in the range between 2.5D and 3.0D. This phenomenon cannot be caught by 2-dimensional analysis.(2) Except for the front face of the rectangular sectioned member, the average pressure coefficient shows a totally different distribution between the 2-dimensional analysis and 3- dimensional analyses. Large fluctuations are observed in the 2-dimensional analysis, and this is one of the factors in the overestimation or underestimation of aerodynamic forces in 2-dimensional analysis.(3) In 2-dimensional analysis, the separation shear layer, which separated at the front edge, reattaches in a position much earlier than the point of reattachment indicated by the wind tunnel tests. Moreover, the pressure fluctuations on the surface are greater because of the greater strength of the vortex formed. This is believed to be one of the causes which produce high-frequency components in the fluctuating lift. The reason fluctuating flow in axial direction cannot be expressed by 2-dimensional analysis is the impossibility of correctly evaluating energy dissipation.

很明显，当通过数值流体流动分析来表达精确的空气动力学特性和矩形截面构件周围的流动状态时，需要在一定雷诺数范围内进行三维分析，其中分离剪切层在前缘分离并重新附着到构件的后表面，如平面箱形梁桥所示。主要结果如下：（1）三维分析有助于定性地了解风洞试验结果所反映的矩形构件的气动特性和绕流状态。此外，在前缘分离的分离剪切层在2.5D和3.0D之间的范围内重新附着。这种现象无法通过二维分析来捕捉。(2)除矩形截面构件的前表面外，二维分析和三维分析的平均压力系数呈现出完全不同的分布。在二维分析中观察到大的波动，这是在二维分析中高估或低估气动力的因素之一。(3)在二维分析中，在前缘分离的分离剪切层在比风洞试验所指出的再附着点早得多的位置上再附着。此外，表面上的压力波动更大，因为形成的涡流强度更大。这被认为是在脉动升力中产生高频分量的原因之一。轴向脉动水流不能用二维分析表示的原因是不能正确地评价消能。