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Lift Distribution on a High Aspect Ratio Circulation Control Wing with Root Lift Cutout

机译：具有根部提升切口的高纵横比循环控制翼上的升力分布

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摘要

A computational procedure is developed, based on lifting line theory, which successfully predicts the spanwise lift distribution at moderate blowing momentum coefficient on a high aspect ratio (AR = 18) circulation control wing-body model with several variations in the spanwise lift distribution which validates this procedure. Additional keywords: Coanda surface; Wing body configurations; Mathematical models. (Author)

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作者
Furey, R. J.;
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年度 1985
页码 p.1-53
总页数 53
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Lift; High lift; Mathematical prediction; Blowers; Coefficients; Momentum; Coanda effect; Surfaces; Aspect ratio; High rate; Theory; Circulation; Wing body configurations; Control; Computations; Distribution; Mathematical models;

机译：升力;高升力;数学预测;鼓风机;系数;动量;柯恩达效应;曲面;纵横比;高速率;理论;循环;翼体配置;控制;计算;分布;数学模型;

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专利

1. Circulation-controlled high-lift wing for small unmanned aerial vehicle [J] . Yasuyuki Yamada, Irina Vasilieva, Akimasa Takayama, ROBOMECH Journal . 2015,第1期

机译：小型无人机的循环控制高升力机翼
2. A CFD Study on Leading Edge Wing Surface Modification of a Low Aspect Ratio Flying wing to Improve Lift Performance [J] . Ramprasadh C., Devanandh V. International journal of micro air vehicles . 2015,第3期

机译：低纵横比飞行机翼前翼表面改性以提高升力性能的CFD研究
3. Root Cutout Effects on the Aerodynamics of a Low-Aspect-Ratio Revolving Wing [J] . Jardin T., David L. AIAA Journal . 2017,第8期

机译：根部切除对低纵横比旋转机翼空气动力学的影响
4. Lift Distributions on Low- Aspect- Ratio Wings at Low Reynolds Numbers for Micro- Air Vehicle Applications [C] . S. Sathaye, J. Yuan, D. Olinger AIAA Guidance, Navigation, and Control Conference ; 22nd Applied Aerodynamics Conference and Exhibit ; AIAA/AAS Astrodynamics Specialist Conference and Exhibit . 2004

机译：低雷诺数低纵横比机翼上的升力分布，适用于微型飞行器应用
5. THEORETICAL DETERMINATION OF THE PRESSURE DISTRIBUTION ON A LIFTING, SUBSONIC DELTA WING OF ARBITRARY ASPECT RATIO. [D] . SWAIN, CARL EUGENE. 1971

机译：从理论上确定任意纵横比的提升亚音速三角翼上的压力分布。
6. On the lift-optimal aspect ratio of a revolving wing at low Reynolds number [O] . T. Jardin, T. Colonius 2018

机译：低雷诺数下旋转翼升力最佳纵横比
7. Circulation-controlled high-lift wing for small unmanned aerial vehicle [O] . Yasuyuki Yamada, Irina Vasilieva, Akimasa Takayama, 2015

机译：小型无人机的循环控制高升力机翼

Lift Distribution on a High Aspect Ratio Circulation Control Wing with Root Lift Cutout

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