| 航空风洞中大气边界层的模拟 |
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| 引用本文： | 罗家泉,李江河.航空风洞中大气边界层的模拟[J].实验流体力学,1989(4). |
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| 作者姓名： | 罗家泉 李江河 |
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| 作者单位： | 南京航空学院
(罗家泉)，南京航空学院(李江河) |
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| 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的基础上,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航空风洞中的风工程试验中。
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| 关 键 词： | 大气边界层 航空风洞模拟 |
THE SIMULATION OF THE ATMOSPHERIC BOUNDARY LAYER IN AN AERONAUTICAL WIND TUNNEL |
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| Luo Jiaquan,Li Jianghe.THE SIMULATION OF THE ATMOSPHERIC BOUNDARY LAYER IN AN AERONAUTICAL WIND TUNNEL[J].Experiments and Measur in Fluid Mechanics,1989(4). |
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| Authors: | Luo Jiaquan Li Jianghe |
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| Institution: | Nanjing Aeronautical Institute |
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| Abstract: | Based on the review of the various artificial acceleratedgrowth methods for boundary layer in aeronauticalwind tunnel,this pap-er suggests a simulated equipment which is suitable for NH-2 modelwind tunnel to generate atmospheric boundary layer and its experimentresults.The experiment results compared with data from some related refe-rences are in good agreement,so that these simulated equipments can beextended to NH-2 aeronautical wind tunnel to use for wind engineeringtest. |
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| Keywords: | atmospheric boundary layer aeronautical wind tunnel simulation |
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