| 测力法在翼型动态失速试验研究中的应用 |
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| 引用本文： | 汤瑞源,赵明亮,吴永健.测力法在翼型动态失速试验研究中的应用[J].实验流体力学,1995(2). |
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| 作者姓名： | 汤瑞源 赵明亮 吴永健 |
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| 作者单位： | 南京航空航天大学 |
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| 摘 要： | 本文就利用测力法对ＮＡＣＡ００１２翼型在振荡条件下的动态失速特性进行的测试作了简要介绍，阐述了测力法在翼型动态实验研究中的一些特殊问题及其解决途径，并比较了两种实验研究方法的优缺点。
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| 关 键 词： | 翼型，振荡，风洞试验，动态失速，力和压力测量 |
THE APPLICATION OF THE FORCE MEASUREMENT METHOD ON EXPERIMENTAL STUDY OF AIRFOIL DYNAMIC STALL |
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| Tang Ruiyuan, Zhao Mingliang,Wu Yongjian.THE APPLICATION OF THE FORCE MEASUREMENT METHOD ON EXPERIMENTAL STUDY OF AIRFOIL DYNAMIC STALL[J].Experiments and Measur in Fluid Mechanics,1995(2). |
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| Authors: | Tang Ruiyuan Zhao Mingliang Wu Yongjian |
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| Institution: | Nanjing University of Aeronautics and Astronautics |
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| Abstract: | The introduction of the force measurement method on experimental study of dynamic stall on the oscillating airfoil NACA0012 is given.Some special questions on the force measurement method and the traditional pressure measurement are discussed. The advantages and the deficiencies of two methods are also discussed. |
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| Keywords: | airfoil oscillation dynamic stall wind tunnel test force measurement and pressure measurement |
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