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Effects of leading-edge radius and maximum thickness-chord ratio on the variation with Mach number of the aerodynamic characteristics of several thin NACA airfoil sections

机译：前缘半径和最大厚度弦比对几种薄NaCa翼型截面气动特性随马赫数变化的影响

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Berggren, Robert E; Graham, Donald J;
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年度 1954
页码 1-67
总页数 67
原文格式 PDF
正文语种 eng
中图分类工业技术;
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2. Comparison of the Aerodynamic Characteristics of the NACA0012 Airfoil at Low-to-Moderate Reynolds Numbers for any Aspect Ratio [J] . S. Martínez-Aranda, A. L. García-González, L. Parras, International Journal of Aerospace Sciences . 2016,第1期

机译：在任何纵横比下，中低雷诺数下NACA0012机翼的空气动力学特性比较
3. Leading-Edge Radius Effects on Aerodynamic Characteristics of 50-Degree Delta Wings [J] . N. G. Verhaagen Journal of Aircraft . 2012,第2期

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4. Effect of Leading-Edge Tubercle on Aerodynamic Performance of NACA 0021 Airfoil [C] . Alok Mishra, Saravana Kumar Lakshmanan, Ashoke De International Conference on Modern Research in Aerospace Engineering . 2018

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5. Aerodynamic performance of transonic and subsonic airfoils: Effects of surface roughness, turbulence intensity, Mach number, and streamline curvature-airfoil shape. [D] . Zhang, Qiang. 2005

机译：跨音速和亚音速机翼的空气动力学性能：表面粗糙度，湍流强度，马赫数和流线曲率翼型的影响。
6. Effects of Leading Edge Defect on the Aerodynamic and Flow Characteristics of an S809 Airfoil [O] . Yan Wang, Xiaojing Zheng, Ruifeng Hu, -1

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7. Effects of Leading-Edge Radius on Aerodynamic Characteristics of 50º Delta Wings [O] . Verhaagen, N.G. 2010

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Effects of leading-edge radius and maximum thickness-chord ratio on the variation with Mach number of the aerodynamic characteristics of several thin NACA airfoil sections

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