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龙脊风帆模型气动特性风洞实验
引用本文:卢占斌,魏庆鼎,王安武.龙脊风帆模型气动特性风洞实验[J].实验流体力学,2001,15(4):46-52.
作者姓名:卢占斌  魏庆鼎  王安武
作者单位:1. 北京大学湍流研究国家重点实验室,北京,100871
2. 天津天保建设发展有限公司,天津,300456
基金项目:自然科学基金资助 ( 5 9895 4 1 0 )
摘    要:通过风洞模型实验 ,利用六分量高频底座天平技术 ,测量了称为龙脊风帆的一种单帆模型在均匀来流中各个风向角和俯仰角下的时均升力系数和时均阻力系数以及脉动升力系数和脉动阻力系数 ,可为工程中类似帆形结构的设计和受力计算提供参考

关 键 词:风荷载  高频底座天平  阻力系数  升力系数
文章编号:1007-3124(2001)04-0046-07
修稿时间:2000年3月6日

A wind tunnel experiment on the aerodynamic character of the dragon-ridge sail model
LU Zhan Bin ,WEI Qing Ding ,WANG An Wu.A wind tunnel experiment on the aerodynamic character of the dragon-ridge sail model[J].Experiments and Measur in Fluid Mechanics,2001,15(4):46-52.
Authors:LU Zhan Bin  WEI Qing Ding  WANG An Wu
Institution:LU Zhan Bin 1,WEI Qing Ding 1,WANG An Wu 2
Abstract:A wind tunnel experiment on a kind of single sail model that is named Dragon Ridge Sail has been conducted. The mean and fluctuating coefficients of drag and lift of the model in various wind directions and pitch angles were obtained through high frequency base balance technique. These results provide references to similar sail shaped constructions in engineering applications.
Keywords:wind load  high frequency base balance  drag coefficient  lift coefficient  
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