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Effect of Mach and Reynolds numbers on the maximum lift coefficient obtainable in gradual and abrupt stalls of a pursuit airplane equipped with a low-drag wing

机译：马赫数和雷诺数对配备低阻翼的追击飞机逐渐和突然失速可获得的最大升力系数的影响

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作者
Blair, William K;
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年度 1945
页码 1-28
总页数 28
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
STALLING - BELL P-63A-6; REYNOLDS NUMBER; MACH NUMBER; AIRPLANES - BELL P-63A-6 FLIGHT TESTS (AMER ); LIFT COEFFICIENTS - BELL P-63A-6;

机译：失速 - BELL p-63a-6; REYNOLDs NUmBER;马赫数;飞机 - 贝尔p-63a-6飞行测试（美国）;提升系数 - BELL p-63a-6;

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1. Mach and Reynolds Number Dependencies of the Stall Behavior of High-Lift Wing-Sections [J] . J. Wild Journal of Aircraft . 2013,第4期

机译：马赫和雷诺数依赖关系的高起重机翼部分失速行为
2. Predicting Maximum Lift Coefficient for Twisted Wings Using Lifting-Line Theory [J] . W. F. Phillips, N. R. Alley Journal of Aircraft . 2007,第3期

机译：基于举升线理论的双翼最大升力系数预测
3. Sectional lift coefficient of a rotating wing at low Reynolds numbers [J] . Kim Jieun, Kweon Jihoon, Choi Haecheon Journal of Mechanical Science and Technology . 2015,第11期

机译：低雷诺数下旋转翼的截面升力系数
4. Experimental investigation of Mach- and Reynolds-number dependencies of the stall behavior of 2-element and 3- element high-lift wing sections [C] . J. Wild AIAA aerospace sciences meeting including the new horizons forum and aerospace exposition . 2012

机译：马赫数和雷诺数依赖关系对2要素和3要素高升力机翼截面失速行为的影响
5. Study of belly-flaps to enhance lift and pitching moment coefficient of a Blended-Wing-Body airplane in landing and takeoff configuration. [D] . Staelens, Yann Daniel. 2007

机译：研究腹部襟翼，以提高降落和起飞配置下的混合机翼机身飞机的升力和俯仰力矩系数。
6. Experimental investigation of Mach- and Reynolds-number dependencies of the stall behavior of 2-element and 3-element high-lift wing sections [O] . Jochen Wild 2012

机译：2元和3元件高升翼段失速行为的马赫和雷诺数依赖性的实验研究

Effect of Mach and Reynolds numbers on the maximum lift coefficient obtainable in gradual and abrupt stalls of a pursuit airplane equipped with a low-drag wing

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