Decoupling wing-shape effects of wing-swept angle and aspect ratio on a forward-flying butterfly

机翼扭转 攻角 机翼载荷 后掠翼 机翼外形 翼尖涡流 冲刷 俯仰角 涡流 阻力 空气动力学 Lift(数据挖掘) 物理 机械 光学 航空航天工程 马蹄涡 涡度 计算机科学 工程类 气象学 数据挖掘 地球物理学
作者
Sheng-Kai Chang,You-Jun Lin,Kuan-Lun Hsu,Jing‐Tang Yang
出处
期刊:Physical review [American Physical Society]
卷期号:107 (6): 065105-065105 被引量:6
标识
DOI:10.1103/physreve.107.065105
摘要

The effect of wing shape on a forward-flying butterfly via decoupled factors of the wing-swept angle and the aspect ratio (AR) was investigated numerically. The wing-shape effect is a major concern in the design of a microaerial vehicle (MAV). In nature, the wing of a butterfly consists of partially overlapping forewing and hindwing; when the forewing sweeps forward or backward relative to the hindwing, the wing-swept angle and the AR of the entire wing simultaneously change. The effects of the wing-swept angle and AR on aerodynamics are coupled. To decouple their effects, we established wing-shape models with varied combinations of the wing-swept angle and AR based on the experimental measurement of two butterfly species (Papilio polytes and Kallima inachus) and developed a numerical simulation for analysis. In each model, the forewing and hindwing overlapped partially, constructing a single wing. Across the models, the wing-swept angle and AR of these single wings varied sequentially. The results show that, through our models, the effects of the wing-swept angle and AR were decoupled; both have distinct flow mechanisms and aerodynamic force trends and are consistent in the two butterfly species. For a fixed AR, a backward-swept wing increases lift and drag because of the enhanced attachment of the leading-edge vortex with increased strength of the wingtip vortex and the spanwise flow. For a fixed wing-swept angle, a small AR wing increases lift and decreases drag because of the large region of low pressure downstream and the wake-capture effect. Coupling these effects, the largest lift-to-drag ratio occurs for a forward-swept wing with the smallest AR. These results indicate that, in a flapping forward flight, sweeping a forewing forward relative to a hindwing is suitable for cruising. The flow mechanisms and decoupled and coupled effects of the wing-swept angle and the AR presented in this paper provide insight into the flight of a butterfly and the design of a MAV.
最长约 10秒,即可获得该文献文件

科研通智能强力驱动
Strongly Powered by AbleSci AI
科研通是完全免费的文献互助平台,具备全网最快的应助速度,最高的求助完成率。 对每一个文献求助,科研通都将尽心尽力,给求助人一个满意的交代。
实时播报
雪意完成签到 ,获得积分10
刚刚
刚刚
我真是坠了完成签到,获得积分10
1秒前
2mo完成签到,获得积分10
1秒前
Tang Yuanfei完成签到 ,获得积分10
3秒前
军军问问张完成签到,获得积分10
3秒前
清秀小凝完成签到,获得积分10
4秒前
眼睛大又蓝完成签到,获得积分10
4秒前
隐形的皮皮虾完成签到,获得积分10
4秒前
欣慰的雨旋完成签到 ,获得积分10
4秒前
hohn完成签到,获得积分10
4秒前
不喝可乐汽水完成签到,获得积分10
5秒前
Untitled应助大胆的致远采纳,获得80
5秒前
6秒前
布同完成签到,获得积分0
7秒前
7秒前
ferritin完成签到 ,获得积分10
8秒前
斯文友琴完成签到,获得积分10
8秒前
Medici完成签到,获得积分10
9秒前
科研通AI6.2应助ZGQ采纳,获得50
9秒前
江郁清完成签到 ,获得积分10
10秒前
妮妮发布了新的文献求助10
10秒前
Wang完成签到,获得积分10
11秒前
突然好想你_1017完成签到,获得积分10
11秒前
打打应助竹简采纳,获得30
11秒前
某某完成签到,获得积分10
11秒前
占临风完成签到,获得积分10
12秒前
第七个南瓜完成签到,获得积分10
12秒前
jijibao完成签到,获得积分10
12秒前
番茄完成签到,获得积分10
12秒前
南霖完成签到,获得积分10
12秒前
啦啦啦完成签到 ,获得积分10
12秒前
帆子完成签到 ,获得积分10
12秒前
村口的帅老头完成签到 ,获得积分10
13秒前
13秒前
14秒前
淡淡映秋完成签到 ,获得积分10
14秒前
15秒前
611完成签到 ,获得积分10
16秒前
复杂妙海完成签到,获得积分10
16秒前
高分求助中
(应助此贴封号)【重要!!请各用户(尤其是新用户)详细阅读】【科研通的精品贴汇总】 10000
An Introduction to Foreign Language Learning and Teaching 750
China Pluperfect I: Epistemology of Past and Outside in Chinese Art 520
Matrix Methods in Data Mining and Pattern Recognition Second Edition 510
Les chinois de jakarta: temples et vie collective 500
The fast track to determining transfer functions of linear circuits: The student guide 500
What is the Future of Psychotherapy in Digital Age? Technology, AI Bots, and Psychotherapy after Covid 444
热门求助领域 (近24小时)
化学 材料科学 医学 生物 纳米技术 工程类 有机化学 化学工程 生物化学 计算机科学 内科学 物理 复合材料 催化作用 细胞生物学 无机化学 光电子学 物理化学 电极 基因
热门帖子
关注 科研通微信公众号,转发送积分 7627630
求助须知:如何正确求助?哪些是违规求助? 9202144
关于积分的说明 19729243
捐赠科研通 7197438
什么是DOI,文献DOI怎么找? 3273859
关于科研通互助平台的介绍 2436196
邀请新用户注册赠送积分活动 2270006