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Development and Evaluation of a Dynamic, 3-Degree-of-Freedom (DOF) Wind Tunnel Model.

机译：动态三自由度（DOF）风洞模型的开发与评估。

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作者
Nelson, B. P.;
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年度 2016
页码 1-36
总页数 36
原文格式 PDF
正文语种 eng
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关键词
Wind tunnel model;

机译：风洞模型;

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2. Development of a Wind Tunnel Test Section for Evaluation of Heavy Vehicle Aerodynamic Drag at a scale of 1:3 [J] . Damien J. McArthur, David Burton, Mark Thompson, SAE International Journal of Commercial Vehicles . 2013,第2期

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3. Recent developments in the calculation of low-speed solid-walled wind tunnel wall interference in tests on large models Part Ⅰ: evaluation of three interference assessment methods [J] . J.E. Hackett Progress in Aerospace Sciences . 2003,第6a7期

机译：大型模型试验中低速实壁风洞墙干扰计算的最新进展第一部分：三种干扰评估方法的评估
4. WIND TUNNEL INVESTIGATION OF CRITICAL FLIGHT REGIMES USING DYNAMICALLY SCALED ACTIVELY CONTROLLED MODEL IN 3 DOF GIMBAL [C] . I. Grishin, A. Khrabrov, A. Kolinko, Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences . 2014

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5. The development of a small scale wind tunnel simulating the atmospheric boundary layer in support of a stochastic wind model. [D] . Hobson-Dupont, Maximillian. 2015

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6. Aerodynamic evaluation of wing shape and wing orientation in four butterfly species using numerical simulations and a low-speed wind tunnel and its implications for the design of flying micro-robots [O] . Alejandro Ortega Ancel, Rodney Eastwood, Daniel Vogt, 2017

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7. 2 Dynamically Improved 6-DOF System for Measurements of Forces and Torques in Wind Tunnels [O] . V. Portman, V. Chapsky 2015

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Development and Evaluation of a Dynamic, 3-Degree-of-Freedom (DOF) Wind Tunnel Model.

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