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Two-dimensional wind tunnel investigation of a symmetrical airfoil section with a sealed internally balanced control surface and a leading tab

机译：对称翼型截面的二维风洞研究，具有密封的内部平衡控制表面和前导片

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Nuber, Robert J; Fullmer, Felicien F , Jr;
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年度 1949
页码 1-43
总页数 43
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Two-Dimensional Wind Tunnel and Computational Investigation of a Microtab Modified Airfoil [J] . J. P. Baker, K. J. Standish, C. P. van Dam Journal of Aircraft . 2007,第2期

机译：微型风翼修饰翼型的二维风洞和计算研究
2. Comparative in-flight and wind tunnel investigation of the development of natural and controlled disturbances in the laminar boundary layer of an airfoil [J] . Inken Peltzer Experiments in Fluids . 2008,第6期

机译：机翼层流边界层中自然扰动和受控扰动发展的空中和风洞比较研究
3. Comparative in-flight and wind tunnel investigation of the development of natural and controlled disturbances in the laminar boundary layer of an airfoil [J] . Peltzer I Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2008,第6期

机译：机翼层流边界层中自然扰动和受控扰动发展的空中和风洞比较研究
4. Two- Dimensional Wind Tunnel and Computational Investigation of a Microtab Modified S809 Airfoil [C] . J. Baker, K. Standish, C. van AIAA Aerospace Sciences Meeting and Exhibit . 2005

机译：Microtab改进型S809机翼的二维风洞和计算研究
5. A two-dimensional transverse vortex wind tunnel for PIV investigation of airfoil vortex interaction. [D] . Brassard, Daniel. 2005

机译：用于机翼旋涡相互作用的PIV研究的二维横向旋涡风洞。
6. Airfoil Selection Procedure Wind Tunnel Experimentation and Implementation of 6DOF Modeling on a Flying Wing Micro Aerial Vehicle [O] . Taimur Ali Shams, Syed Irtiza Ali Shah, Ali Javed, 2020

机译：翼型微型飞行器的机翼选择程序风洞实验和6DOF建模实现
7. Wind tunnel testing of an airfoil with a moving surface boundary-layer control. [O] . Al-Garni Abdullah Mohammed 1999

机译：具有移动表面边界层控制的翼型的风洞测试。

Two-dimensional wind tunnel investigation of a symmetrical airfoil section with a sealed internally balanced control surface and a leading tab

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