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Effects of 45 deg Sweepback on the High-Speed Characteristics of a Wing Having a Modified NACA 16-012 Airfoil Section

机译：在翼具有修饰的NaCa 16-012翼剖面的高速特性45度后掠角的影响。

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作者
Liccini, L. L.;
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年度 1947
页码 p.1-29
总页数 29
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Airfoils ; Sweptback wings ; Wind tunnel tests ; High velocity;

机译：机翼，后掠翼;风洞试验;高速度;

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1. Experimental Analysis of a NACA 0021 Airfoil Section Through 180-Deg Angle of Attack at Low Reynolds Numbers for Use in Wind Turbine Analysis [J] . Holst D., Church B., Pechlivanoglou G., Journal of Engineering for Gas Turbines and Power . 2019,第4期

机译：用于风力涡轮机分析的低雷诺数下NACA 0021翼型截面通过180度迎角的实验分析
2. Rarefied gas flow simulations of NACA 0012 airfoil and sharp 25-55-deg biconic subject to high order nonequilibrium boundary conditions in CFD [J] . Nam T.P. Le, Ahmad Shoja-Sani, Ehsan Roohi Aerospace science and technology . 2015,第feba期

机译：在CFD中高阶非平衡边界条件下，NACA 0012机翼和锋利的25-55度双锥齿轮的稀疏气流模拟
3. Magnus effect on Aerodynamic Characteristics on Wing Airfoil MH45 [J] . S. Ketan, P. Vishal, R. Sundeep, International journal of comadem . 2018,第1期

机译：马格努斯对翼型MH45气动特性的影响
4. Effect of trailing edge serration on the lift and drag characteristics of NACA0012 airfoil wing [C] . Usama Hussain, Saif Ul Malook, Burhan Shabir, AIAA applied aerodynamics conference;AIAA Aviation Forum . 2017

机译：后缘锯齿对NACA0012机翼机翼升力和阻力特性的影响
5. DETERMINATION OF THE LOCAL HEAT TRANSFER CHARACTERISTICS OF GLAZE-ICE ACCRETIONS ON A CYLINDER AND A NACA 0012 AIRFOIL. [D] . PAIS, MARTIN RABINDRA. 1987

机译：确定汽缸和NACA 0012机翼上的冰结垢的局部传热特性。
6. Effects of Leading Edge Defect on the Aerodynamic and Flow Characteristics of an S809 Airfoil [O] . Yan Wang, Xiaojing Zheng, Ruifeng Hu, -1

机译：前缘缺陷对S809翼型气动和流动特性的影响
7. Wind tunnel tests of the NACA 63-415 and a modified NACA 63-415 airfoil [O] . Bak C., Fuglsang P., Johansen J., 2000

机译：NaCa 63-415和改进的NaCa 63-415翼型的风洞试验

Effects of 45 deg Sweepback on the High-Speed Characteristics of a Wing Having a Modified NACA 16-012 Airfoil Section

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