Literature DB >> 19258688

Size effects on insect hovering aerodynamics: an integrated computational study.

H Liu1, H Aono.   

Abstract

Hovering is a miracle of insects that is observed for all sizes of flying insects. Sizing effect in insect hovering on flapping-wing aerodynamics is of interest to both the micro-air-vehicle (MAV) community and also of importance to comparative morphologists. In this study, we present an integrated computational study of such size effects on insect hovering aerodynamics, which is performed using a biology-inspired dynamic flight simulator that integrates the modelling of realistic wing-body morphology, the modelling of flapping-wing and body kinematics and an in-house Navier-Stokes solver. Results of four typical insect hovering flights including a hawkmoth, a honeybee, a fruit fly and a thrips, over a wide range of Reynolds numbers from O(10(4)) to O(10(1)) are presented, which demonstrate the feasibility of the present integrated computational methods in quantitatively modelling and evaluating the unsteady aerodynamics in insect flapping flight. Our results based on realistically modelling of insect hovering therefore offer an integrated understanding of the near-field vortex dynamics, the far-field wake and downwash structures, and their correlation with the force production in terms of sizing and Reynolds number as well as wing kinematics. Our results not only give an integrated interpretation on the similarity and discrepancy of the near- and far-field vortex structures in insect hovering but also demonstrate that our methods can be an effective tool in the MAVs design.

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Year:  2009        PMID: 19258688     DOI: 10.1088/1748-3182/4/1/015002

Source DB:  PubMed          Journal:  Bioinspir Biomim        ISSN: 1748-3182            Impact factor:   2.956


  13 in total

1.  Aerodynamic performance of a hovering hawkmoth with flexible wings: a computational approach.

Authors:  Toshiyuki Nakata; Hao Liu
Journal:  Proc Biol Sci       Date:  2011-08-10       Impact factor: 5.349

2.  Indirect actuation reduces flight power requirements in Manduca sexta via elastic energy exchange.

Authors:  Jeff Gau; Nick Gravish; Simon Sponberg
Journal:  J R Soc Interface       Date:  2019-12-18       Impact factor: 4.118

3.  A CFD-informed quasi-steady model of flapping wing aerodynamics.

Authors:  Toshiyuki Nakata; Hao Liu; Richard J Bomphrey
Journal:  J Fluid Mech       Date:  2015-11       Impact factor: 3.627

4.  Aerodynamic characteristics of the ventilated design for flapping wing micro air vehicle.

Authors:  G Q Zhang; S C M Yu
Journal:  ScientificWorldJournal       Date:  2014-02-06

5.  Multiple leading edge vortices of unexpected strength in freely flying hawkmoth.

Authors:  L Christoffer Johansson; Sophia Engel; Almut Kelber; Marco Klein Heerenbrink; Anders Hedenström
Journal:  Sci Rep       Date:  2013-11-20       Impact factor: 4.379

6.  Clap-and-fling mechanism in a hovering insect-like two-winged flapping-wing micro air vehicle.

Authors:  Hoang Vu Phan; Thi Kim Loan Au; Hoon Cheol Park
Journal:  R Soc Open Sci       Date:  2016-12-07       Impact factor: 2.963

7.  Wing kinematics in a hovering dronefly minimize power expenditure.

Authors:  J H Wu; M Sun
Journal:  J Insect Sci       Date:  2014-10-15       Impact factor: 1.857

Review 8.  Study of Mosquito Aerodynamics for Imitation as a Small Robot and Flight in a Low-Density Environment.

Authors:  Balbir Singh; Noorfaizal Yidris; Adi Azriff Basri; Raghuvir Pai; Kamarul Arifin Ahmad
Journal:  Micromachines (Basel)       Date:  2021-05-02       Impact factor: 2.891

Review 9.  Biomechanics and biomimetics in insect-inspired flight systems.

Authors:  Hao Liu; Sridhar Ravi; Dmitry Kolomenskiy; Hiroto Tanaka
Journal:  Philos Trans R Soc Lond B Biol Sci       Date:  2016-09-26       Impact factor: 6.237

10.  The leading-edge vortex on a rotating wing changes markedly beyond a certain central body size.

Authors:  Shantanu S Bhat; Jisheng Zhao; John Sheridan; Kerry Hourigan; Mark C Thompson
Journal:  R Soc Open Sci       Date:  2018-07-11       Impact factor: 2.963

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