Effects of wing–body interaction on hawk moth aerodynamics and energetics at various flight velocities

Author:

Xue Yujing12,Cai Xuefei12,Liu Hao12ORCID

Affiliation:

1. Shanghai Jiao Tong University and Chiba University International Cooperative Research Center (SJTU-CU ICRC), 800 Dongchuan Road, Minhang District, Shanghai 200240, People's Republic of China

2. Graduate School of Engineering, Chiba University, 1-33, Yayoi-cho, Inage-ku, Chiba 263-8522, Japan

Abstract

Although the aerodynamics and energetics associated with single or paired flapping wings of insects have attracted significant attention, the aerodynamic interaction between the flapping wings and the flying body as a function of flight velocity remains an open question. Here, we present a computational fluid dynamic (CFD) study of hawk moth aerodynamics and energetics for hovering and forward flights of five different velocities. We build up a high-fidelity CFD wing–body (WB) model based on the realistic morphology and the WB kinematics of hawk moth Manduca sexta, which enables trimmed flapping flights based on a genetic algorithm embedded within a CFD-driven model. The effects of WB interactions on velocity-dependent aerodynamic performance are examined with WB, wing–wing, and body-only models in terms of leading-edge-vortex- and body-vortex-based mechanisms and their correlations with the production of aerodynamic forces and power consumption. While leading-edge-vortices are a convergent mechanism responsible for creating most of the aerodynamic force, the body-vortices created by WB interactions can augment the vertical force at all flight velocities, producing a 10% increase in fast flights. The time-averaged body-mass-specific mechanical power produces a J-shaped curve, which lowers power costs in intermediate- and high-velocity flights and saves energy from the WB interaction. An extensive investigation into aerodynamics and power consumption shows that high aspect-ratio wings increase wing- and body-based vertical forces, realistic wing-to-body mass ratios lead to low power costs, and slightly lower reduced frequency optimizes the aerodynamic performance. These results may help us to guide the design of future biomimetic flapping micro-aerial vehicles.

Funder

Japan Society for the Promotion of Science

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3