ON RESULTS'ACCURACY AT TWO-DIMENSIONAL WIND TUNNEL TESTING

机译：二维风洞测试结果准确性的研究

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The principal factors which influence the accuracy of two-dimensional wind tunnel test results are analyzed. The influences of Reynolds number, Mach number and wall interference with reference to solid and flow blockage (blockage of wake) as well as the influence of side-wall boundary layer control are analyzed.

机译：分析了影响二维风洞试验结果准确性的主要因素。分析了雷诺数，马赫数和壁面干扰对固体和流动阻塞（尾流阻塞）的影响，以及侧壁边界层控制的影响。

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《Congress of the International Council of the Aeronautical Sciences;ICAS 2008》|2008年|2309-2318|共10页
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作者
Bosko Rasuo;
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正文语种
中图分类航空;
关键词
wind tunnel testing; interference effects;

机译：风洞测试;干扰效应;

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专利

1. Scaling between Wind Tunnels-Results Accuracy in Two-Dimensional Testing [J] . Bosko Rasuo Transactions of the Japan society for aeronautical and space sciences . 2012,第2期

机译：风洞之间的缩放-二维测试中的结果精度
2. Validation Testing of the Prediction Accuracy of the Numerical Wind Synopsis Prediction Technique RIAM-COMPACT_® for the Case of the Bolund Experiment : Comparison against a Wind-Tunnel Experiment [J] . Takanori UCHIDA 九州大学应用力学研究所所報 . 2014,第147期

机译：数值模拟天气预测技术RIAM-COMPACT_®在Bolund实验中的预测准确性的验证测试：与风洞实验的比较
3. The influence of Reynolds and Mach numbers on two-dimensional wind-tunnel testing: An experience [J] . B. Rasuo The Aeronautical Journal . 2011,第1166期

机译：雷诺数和马赫数对二维风洞测试的影响：经验
4. On Results’ Accuracy at Two-Dimensional Wind Tunnel Testing [C] . Bosko Rasuo New beginnings: challenges for aerospace innovation . 2009

机译：二维风洞测试中结果的准确性
5. Development of a wind tunnel test apparatus for horizontal axis wind turbine rotor testing [D] . McWilliam, Michael K. 2008

机译：用于水平轴风力涡轮机转子测试的风洞测试设备的开发
6. Wind Tunnel Tests for Wind Pressure Distribution on Gable Roof Buildings [O] . Xiao-kun Jing, Yuan-qi Li 2013

机译：在山墙屋顶建筑物上进行风压分布的风洞测试
7. Two-dimensional wind tunnel tests of the SSS series 1 structurally efficient aerofoils for wind turbines [O] . Turnock S.R. 1989

机译：用于风力涡轮机的sss系列1结构高效翼型的二维风洞试验
8. Wind-tunnel Tests on an Aircraft Designed for Supersonic Speeds PART I High-speed Wind-tunnel Tests on 1/6.15-Scale Model Aircraft PART II No. 2 II1/2 -ft. Wind-tunnel Tests on a 1/4-Scale Model Wing [R] . S. P. HUTTON, M. Eng., A. D. Young 1950

机译：针对超音速设计的飞机的风洞测试第一部分1 / 6.15比例模型飞机的高速风洞试验第II部分第2号II1 / 2英尺。风洞测试1/4比例模型翼

ON RESULTS'ACCURACY AT TWO-DIMENSIONAL WIND TUNNEL TESTING

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