Aerodynamics of dragonfly flight

The material property, kinematics and computational fluid dynamics of the dragonfly Sympetrum flaveolum are investigated. The elastic modulus of the leading edge spar of a hindwing, obtained through vibration tests, was found to be similar to rubber with small strain. The flapping motions of the hin...

Full description

Saved in:
Bibliographic Details
Main Author: Chen, Yahui.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Theses and Dissertations
Language:English
Published: 2012
Subjects:
Online Access:http://hdl.handle.net/10356/50671
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Nanyang Technological University
Language: English
id sg-ntu-dr.10356-50671
record_format dspace
spelling sg-ntu-dr.10356-506712023-03-11T17:36:26Z Aerodynamics of dragonfly flight Chen, Yahui. School of Mechanical and Aerospace Engineering Martin Skote DRNTU::Engineering::Mechanical engineering::Fluid mechanics The material property, kinematics and computational fluid dynamics of the dragonfly Sympetrum flaveolum are investigated. The elastic modulus of the leading edge spar of a hindwing, obtained through vibration tests, was found to be similar to rubber with small strain. The flapping motions of the hindwing are recorded using high-speed videography. Two distinct flapping patterns are revealed as a simple figure-eight (S8) and a double figure-eight (D8). The in-flight kinematic models of the two flapping patterns are integrated into the computational fluid dynamic model of a live-sized dragonfly hindwing. The computed aerodynamic force and flow information reveals better aerodynamic performances in D8 than in S8. Most importantly, we propose two new lift enhancing mechanisms through the simulations: (1) increasing the amount of the reduction of the translational acceleration during wing rotations; (2) forming of the vortex tube to stabilise the vortices around the wing to prevent shedding. Doctor of Philosophy (MAE) 2012-08-27T07:47:05Z 2012-08-27T07:47:05Z 2012 2012 Thesis Chen, Y. (2012). Aerodynamics of dragonfly flight. Doctoral thesis, Nanyang Technological University, Singapore. http://hdl.handle.net/10356/50671 en 122 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Mechanical engineering::Fluid mechanics
spellingShingle DRNTU::Engineering::Mechanical engineering::Fluid mechanics
Chen, Yahui.
Aerodynamics of dragonfly flight
description The material property, kinematics and computational fluid dynamics of the dragonfly Sympetrum flaveolum are investigated. The elastic modulus of the leading edge spar of a hindwing, obtained through vibration tests, was found to be similar to rubber with small strain. The flapping motions of the hindwing are recorded using high-speed videography. Two distinct flapping patterns are revealed as a simple figure-eight (S8) and a double figure-eight (D8). The in-flight kinematic models of the two flapping patterns are integrated into the computational fluid dynamic model of a live-sized dragonfly hindwing. The computed aerodynamic force and flow information reveals better aerodynamic performances in D8 than in S8. Most importantly, we propose two new lift enhancing mechanisms through the simulations: (1) increasing the amount of the reduction of the translational acceleration during wing rotations; (2) forming of the vortex tube to stabilise the vortices around the wing to prevent shedding.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Chen, Yahui.
format Theses and Dissertations
author Chen, Yahui.
author_sort Chen, Yahui.
title Aerodynamics of dragonfly flight
title_short Aerodynamics of dragonfly flight
title_full Aerodynamics of dragonfly flight
title_fullStr Aerodynamics of dragonfly flight
title_full_unstemmed Aerodynamics of dragonfly flight
title_sort aerodynamics of dragonfly flight
publishDate 2012
url http://hdl.handle.net/10356/50671
_version_ 1761781304069718016