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Experimental and Calculated Characteristics of Three Wings of NACA 64- 210 and 65-210 Airfoil Sections with and without 2 deg Washout

机译：NaCa 64- 210的三个翼和65-210翼型断面具有和不具有2度冲蚀试验的和计算特征

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作者
Sivells, J. C.;
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作者单位

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年度 1947
页码 1-1
总页数 1
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Wings ; Aerodynamics ; Airfoils;

机译：翼;空气动力学;机翼;

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1. Free vibration analysis of composite aircraft wings modeled as thin-walled beams with NACA airfoil sections [J] . Thin-Walled Structures . 2019,第Juna期

机译：具有NACA翼型截面的薄壁梁模型的复合材料飞机机翼的自由振动分析
2. 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
3. Experimental Investigation of Near-Field Aeroacoustic Characteristics of a Pre- and Post-Stall NACA 65-410 Airfoil [J] . Zang B., Mayer Yannick D., Azarpeyvand Mahdi Journal of aerospace engineering . 2021,第6期

机译：预测和后纳卡65-410翼型近场气流特性的实验研究
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. The Effect of Attack Angle On The Vibration Suppression Of Composite Wing Airfoil NACA 0012 [O] . Hassan Ali Kadhem, Ahmed Abdul Hussein 2021

机译：攻击角对复合翼翼翼型Naca 0012振动抑制的影响

Experimental and Calculated Characteristics of Three Wings of NACA 64- 210 and 65-210 Airfoil Sections with and without 2 deg Washout

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