3-Dimensional Fluid Flow Analysis for Aerodynamic Response Characteristics of Rectangular Cylinder
3-Dimensional Fluid Flow Analysis for Aerodynamic Response Characteristics of Rectangular Cylinder
批准号:
09650533
负责人:
HIRANO Hirokazu
金额:
$1.66万
依托单位:
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
项目状态:
已结题
起止时间:
1997 至 1999
中文摘要
以平面箱梁桥为例,用数值流体流动分析来表达分离剪切层前缘分离并重新附着于构件后表面的矩形截面构件的精确气动特性和流动状态时,需要在一定雷诺数范围内进行三维分析。主要结果如下:(1)三维分析有助于定性地理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。在2.5D ~ 3.0D范围内,在前缘分离的分离剪切层重新附着。这种现象不能被二维分析捕捉到。(2)除矩形截面构件前端面外,平均压力系数在二维分析和三维分析中表现出完全不同的分布。在二维分析中观察到较大的波动,这是造成二维分析中气动力估计过高或过低的因素之一。(3)在二维分析中,在前缘分离的分离剪切层在比风洞试验显示的再附着点更早的位置重新附着。此外,由于形成的涡流强度越大,表面压力波动也越大。这被认为是在波动升力中产生高频分量的原因之一。轴向波动流不能用二维分析来表示的原因是不能正确地计算能量耗散。
英文摘要
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.
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平野・渡辺・丸岡・佐野: "断面辺長比4の矩形断面の空力特性に関する2次元・3次元数値流体解析" 土木学会論文集. Vol.598 I-44. 401-411 (9807)
Hirano、Watanabe、Maruoka、Sano:“边长比为 4 的矩形横截面空气动力特性的二维和三维数值流体分析”日本土木工程师学会论文集第 598 卷 I-44。 401-411 (9807)
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作者:
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通讯作者:
丸岡晃,平野廣和,志村正幸: "多数本角柱まわりの数値流体解析を行うための境界条件とモデル化の検討"土木学会・応用力学論文集. 2号. 567-572 (1999)
Akira Maruoka、Hirokazu Hirano、Masayuki Shimura:“多棱镜周围计算流体分析的边界条件和建模研究”,日本土木工程学会应用力学杂志,第 2 期,567-572 (1999)
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平野・渡辺・丸岡: "矩形断面の空力特性に及ぼすレイノルズ数の影響" 土木学会応用力学論文集. Vol.1. 655-663 (9809)
Hirano、Watanabe 和 Maruoka:“雷诺数对矩形横截面空气动力学特性的影响”,日本土木工程师学会应用力学杂志,第 1 卷 655-663 (9809)。
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渡辺茂・平野廣和: "剥離・再付着型矩形断面の流れ特性に関する数値解析" 土木学会第52回年次学術講演会. 1-B. 18-19 (1997)
Shigeru Watanabe 和 Hirokazu Hirano:“剥离和再附着矩形横截面流动特性的数值分析”日本土木工程师学会第 52 届学术年会 18-B(1997)。
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通讯作者:
平野、渡邊、丸岡: "Aerodynamic Characteristics of Rectangular Cylinders"Journal of Computational Fluid Dynamics. 12. 151-163 (1999)
Hirano、Watanabe、Maruoka:“矩形圆柱体的空气动力学特性”计算流体动力学杂志。12. 151-163 (1999)
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共 22 条
Research on the cause investigation of the reservoir damaged by bulging phenomenon and its vibration control measures
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批准号:16K06473
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$3.0万
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财政年份:2016
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负责人:HIRANO Hirokazu
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Research on Sloshing Measures of Estimation of Overflowed Liquid and Control Method with Damping Device
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资助金额:$2.83万
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财政年份:2010
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Experiment method proposal on sloshing behavior of real scale floating-roof-tank
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批准号:19560486
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项目类别:Grant-in-Aid for Scientific Research (C)
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财政年份:2007
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负责人:HIRANO Hirokazu
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依托单位:
Calculations of Unsteady Aerodynamic Forces using Computational Fluid Dynamics and Wind Tunnel Test.
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批准号:13650532
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$2.11万
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财政年份:2001
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负责人:HIRANO Hirokazu
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依托单位:
Numerical Fluid Flow Analysis for Aerodynamic Response Characteristics to Safety Desing of Wind Resistance of Grate Structure
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批准号:06650526
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$1.28万
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财政年份:1994
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负责人:HIRANO Hirokazu
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依托单位:
海外基金