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Aerodynamic Characteristics of a Variable Span Wing Flying Inside a Channel I (Effects of Wing Aspect Ratio and Guideway)

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）

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Cheolheui Han;
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1. 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
2. Aerodynamic and Static Aeroelastic Characteristics of a Variable-Span Morphing Wing [J] . Jae-Sung Bae, T. Michael Seigler, Daniel J. Inman Journal of Aircraft . 2005,第2期

机译：变跨距变形翼的气动和静态气动弹性特征
3. Steady Aerodynamic Characteristics of a Wing Flying Over a Nonplanar Ground Surface Part II: Channel [J] . Cheolheui Han, Hakki Kim, Jinsoo Cho Journal of Mechanical Science and Technology . 2006,第7期

机译：飞行在非平面地面上的机翼的稳定气动特性第二部分：通道
4. Adaptive Control Laws for Flexible Semi- Span Wind Tunnel Model of High- Aspect Ratio Flying Wing [C] . I. Gregory, C. Cao, V. Patel, AIAA Guidance, Navigation and Control Conference and Exhibit;AIAA Modeling and Simulation Technologies Conference and Exhibit;AIAA Atmospheric Flight Mechanics Conference and Exhibit . 2007

机译：高纵横比飞行翼柔性半跨风洞模型的自适应控制律
5. Effects of Wing Morphology on Flapping-wing Aerodynamics [D] . Fu, Junjiang. 2017

机译：机翼形态对襟翼空气动力学的影响
6. Aerodynamic evaluation of wing shape and wing orientation in four butterfly species using numerical simulations and a low-speed wind tunnel and its implications for the design of flying micro-robots [O] . Alejandro Ortega Ancel, Rodney Eastwood, Daniel Vogt, 2017

机译：利用数值模拟和低速风洞对四种蝶类的翼形和翼向进行空气动力学评估及其对飞行微型机器人设计的启示
7. Table 2: Values of body mass (Mb), wing span (B), lift surface (SL), aspect ratio (AR), and wing loading (WL) estimated for six bohaiornithid specimens using multiple regressions derived on modern flying birds (see Methods). [O] . -1

机译：表2：体重（MB）的值，翼跨度（B），升降表面（SL），纵横比（AR），以及使用在现代飞鸟上衍生的多元回归估计的六个BohaiornidId标本的翼装（WL）（见方法）。
8. Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch [R] . Driver, Cornelius, Robinson, Ross B 1952

机译：上音调的空气动力特性的掠角和厚度比的作用：在一系列具有为3.5的纵横比和0.2的锥度比弧形翼翼身组合的超音速气动特性

Aerodynamic Characteristics of a Variable Span Wing Flying Inside a Channel I (Effects of Wing Aspect Ratio and Guideway)

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