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航空风洞中大气边界层的模拟
引用本文:李江河 ,罗家泉.航空风洞中大气边界层的模拟[J].南京航空航天大学学报,1988(4).
作者姓名:李江河  罗家泉
摘    要:本文在评述航空风洞中各种人工加速形成边界层方法曲基础上,提出一种适用于NH-2模型风洞形成大气边界层的模拟装置及其试验结果。试验结果与有关资料比较是相符的。故此模拟装置可推广应用到NH-2航空风洞中的风力工程试验。

关 键 词:风洞试验  风力  大气边界层  模拟装置

The Simulation of the Atmospheric Boundary Layer in an Aeronautical Wind Tunnel
Li Jianghe Luo Jiaquan.The Simulation of the Atmospheric Boundary Layer in an Aeronautical Wind Tunnel[J].Journal of Nanjing University of Aeronautics & Astronautics,1988(4).
Authors:Li Jianghe Luo Jiaquan
Institution:Li Jianghe Luo Jiaquan
Abstract:Based on the review of the various artificial accelerated growth methods for boundary layer in aeronautical wind tunnels, this paper suggests a simulated device suitable for NH-2 model wind tunnel to produce atmospheric boundary layer and gives its experimental results.The experimental results, compared with the data from some related references, are in good agreement, so the Simulated device can be extended to NH-2 aeronautical wind tunnel for wind engineering tests.
Keywords:wind tunnel tests  wind force  atmospheric boundary layer  simulated device    
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