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Investigation of the variation of lift coefficient with Reynolds number at a moderate angle of attack on a low-drag airfoil

机译：低阻力翼型中等迎角雷诺数随升力系数变化的研究

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Tetervin, Neal;
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年度 1942
页码 1-8
总页数 8
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
PHOTOGRAPHY - AIR FLOW - AIRFOILS LAMPBLACK; PRESSURE DISTRIBUTION - AIRFOILS - NACA 66,2-216; BOUNDARY LAYER SEPARATION - AIRFOILS; BOUNDARY LAYER - VELOCITY DISTRIBUTION; AIRFOILS - ANGLE OF ATTACK; REYNOLDS NUMBER; LIFT COEFFICIENTS - AIRFOILS; AIRFOILS - NACA 66,2-216 - CHARACTERISTICS LOW-DRAG; WIND TUNNEL TESTS - NACA - LOW-TURBULENCE (7 1/2' X 3');

机译：摄影 - 空气流动 - 飞机灯罩;压力分布 - 翼型 - NaCa 66,2-216;边界层分离 - 飞机;边界层 - 速度分布;机翼 - 攻击角度; REYNOLDs NUmBER;提升系数 - 翼型; aIRFOILs - NaCa 66,2-216 - 特点低拖;风洞测试 - NaCa - 低湍流（7 1/2'X 3'）;

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Investigation of the variation of lift coefficient with Reynolds number at a moderate angle of attack on a low-drag airfoil

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