Computational fluid dynamics of flapping wings

The following final year project presents the computational fluid dynamics simulation of flapping mechanism using the commercial software, FLUENT. It is of the interest to seek understanding of how natural flyers could generate sufficient lift for carrying its own weight during flapping flight....

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Bibliographic Details
Main Author: Chin, Yao Wei.
Other Authors: Jorg Uwe Schluter
Format: Final Year Project (FYP)
Language:English
Published: 2010
Subjects:
Online Access:http://hdl.handle.net/10356/40584
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author Chin, Yao Wei.
author2 Jorg Uwe Schluter
author_facet Jorg Uwe Schluter
Chin, Yao Wei.
author_sort Chin, Yao Wei.
collection NTU
description The following final year project presents the computational fluid dynamics simulation of flapping mechanism using the commercial software, FLUENT. It is of the interest to seek understanding of how natural flyers could generate sufficient lift for carrying its own weight during flapping flight. An overview of basic flapping aerodynamics is given at first before examining the computational approach in FLUENT to simulate air flow around an obstacle. Simulations of vortex shedding from stationary cylinder are carried out at Reynolds number of 20, 40, and 80 to look into the role of vortices in lift generation. The project then continues with simulation of an oscillating cylinder at Re =10000 to model the plunging motion during flapping flights at different frequencies. Lastly, simulations of a pitching plate at Reynolds number of 21000 is carried out for different turbulence model to examine the lift generation mechanism by rotational motion when the wings pitch during flapping flight.
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spelling ntu-10356/405842023-03-04T18:53:01Z Computational fluid dynamics of flapping wings Chin, Yao Wei. Jorg Uwe Schluter School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering::Aerodynamics The following final year project presents the computational fluid dynamics simulation of flapping mechanism using the commercial software, FLUENT. It is of the interest to seek understanding of how natural flyers could generate sufficient lift for carrying its own weight during flapping flight. An overview of basic flapping aerodynamics is given at first before examining the computational approach in FLUENT to simulate air flow around an obstacle. Simulations of vortex shedding from stationary cylinder are carried out at Reynolds number of 20, 40, and 80 to look into the role of vortices in lift generation. The project then continues with simulation of an oscillating cylinder at Re =10000 to model the plunging motion during flapping flights at different frequencies. Lastly, simulations of a pitching plate at Reynolds number of 21000 is carried out for different turbulence model to examine the lift generation mechanism by rotational motion when the wings pitch during flapping flight. Bachelor of Engineering (Aerospace Engineering) 2010-06-16T08:54:24Z 2010-06-16T08:54:24Z 2010 2010 Final Year Project (FYP) http://hdl.handle.net/10356/40584 en Nanyang Technological University 69 p. application/pdf
spellingShingle DRNTU::Engineering::Aeronautical engineering::Aerodynamics
Chin, Yao Wei.
Computational fluid dynamics of flapping wings
title Computational fluid dynamics of flapping wings
title_full Computational fluid dynamics of flapping wings
title_fullStr Computational fluid dynamics of flapping wings
title_full_unstemmed Computational fluid dynamics of flapping wings
title_short Computational fluid dynamics of flapping wings
title_sort computational fluid dynamics of flapping wings
topic DRNTU::Engineering::Aeronautical engineering::Aerodynamics
url http://hdl.handle.net/10356/40584
work_keys_str_mv AT chinyaowei computationalfluiddynamicsofflappingwings