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翼型边界层及近场尾流的湍流特性与气动噪声特性相关规律试验研究
引用本文:白存儒,何克敏,武延祥,郭渠渝.翼型边界层及近场尾流的湍流特性与气动噪声特性相关规律试验研究[J].实验流体力学,2000,14(1):81-84.
作者姓名:白存儒  何克敏  武延祥  郭渠渝
作者单位:西北工业大学,陕西,西安,710072
基金项目:国防基金!( 96J1 3.1 .2 HK0 353)
摘    要:变湍流度试验结果表明 ,湍流度对翼型边界层和尾流的湍流特性、转捩情况、气动噪声特性及其它们间的相关特性有显著影响。这种影响有一定规律。笔者得出了苦干有价值的半经验关系式。

关 键 词:翼型  湍流特性  气动噪声特性  风洞实验
修稿时间:1999-07-20

The experimental investigation of the correlation of turbulent characteristics and aerodynamic noise characteristics of the boundary layer and near wake of an airfoil
BAI Cun-ru,HE Ke-min,WU Yan-xiang,GUO Qu-yu.The experimental investigation of the correlation of turbulent characteristics and aerodynamic noise characteristics of the boundary layer and near wake of an airfoil[J].Experiments and Measur in Fluid Mechanics,2000,14(1):81-84.
Authors:BAI Cun-ru  HE Ke-min  WU Yan-xiang  GUO Qu-yu
Abstract:The test results at variable wind tunnel turbulence shown that the turbulence level has large effects on turbulent characteristics, transition characteristics, aerodynamic noise characteristic and its correlation of the boundary layer and near wake of an airfoil. The effect of turbulence has certain rule. This paper give some Semi Empirical Relations.
Keywords:Variable turbulence  airfoil  turbulent characteristic  aerodynamic noise characteristic  Wind Tunnel Test
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