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The effects of centrally mounted wing-tip tanks on the subsonic aerodynamic characteristics of a wing of aspect ratio 10 with 35 degrees of sweepback

机译：中心安装的翼尖坦克对纵横比为10的翼的亚音速空气动力学特性的影响，具有35度的后掠

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作者
Tinling, Bruce E; Kolk, W Richard;
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年度 1951
页码 1-47
总页数 47
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. A Study on Improvement of Aerodynamic Characteristics of the Next- Generation SST Wing by Lateral Blowing in Subsonic Flow [J] . Makoto Kamishita, Shigeru Aso, Keiichi Karashima 日本航空宇宙学会論文集 . 2001,第569期

机译：亚音速流侧吹改善下一代SST机翼气动特性的研究
2. A Study on Improvement of Aerodynamic Characteristics of the Next- Generation SST Wing by Lateral Blowing in Subsonic Flow [J] . Makoto Kamishita, Shigeru Aso, Keiichi Karashima 日本航空宇宙学会論文集 . 2001,第569期

机译：亚音速流侧吹改善下一代SST机翼气动特性的研究
3. Effects of wing shape, aspect ratio and deviation angle on aerodynamic performance of flapping wings in hover [J] . Shahzad Aamer, Tian Fang-Bao, Young John, Physics of fluids . 2016,第11期

机译：机翼形状，纵横比和偏角对悬停时拍动机翼气动性能的影响
4. Simulation and Sensitivity Analysis of a Wing-Tip Mounted Propeller Configuration from the Workshop for Integrated Propeller Prediction (WIPP) [C] . Beckett Y. Zhou, Nicolas R. Gauger, Myles Morelli, AIAA Aviation Forum . 2020

机译：集成螺旋桨预测车间翼尖安装螺旋桨配置的仿真与敏感性分析（WIPP）
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. Aerodynamic Characteristics of a Variable Span Wing Flying Inside a Channel I (Effects of Wing Aspect Ratio and Guideway) [O] . Cheolheui Han 2016

机译：一种可变跨度翼飞在通道I内的空气动力学特性（机翼纵横比和导轨的效果）

The effects of centrally mounted wing-tip tanks on the subsonic aerodynamic characteristics of a wing of aspect ratio 10 with 35 degrees of sweepback

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