Flapping-flight (I): development of a DC motor-based resonant flapping mechanism for large wing strokes

This study addresses quantifying the performance of an insect-inspired flapping wing prototype under vacuum condition. The flapping motion was produced by using a single electric motor. Instead of exposing in a vacuum condition, the wings of the flapping prototype were replaced by a pair of rigid cy...

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Bibliographic Details
Main Author: Muhammad Hazwan Ismail.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Final Year Project (FYP)
Language:English
Published: 2012
Subjects:
Online Access:http://hdl.handle.net/10356/50287
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author Muhammad Hazwan Ismail.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Muhammad Hazwan Ismail.
author_sort Muhammad Hazwan Ismail.
collection NTU
description This study addresses quantifying the performance of an insect-inspired flapping wing prototype under vacuum condition. The flapping motion was produced by using a single electric motor. Instead of exposing in a vacuum condition, the wings of the flapping prototype were replaced by a pair of rigid cylindrical members that give comparable inertia yet with negligible drag force or aerodynamic damping to achieve the equivalent vacuum environment. For both of the setups, with wings and cylindrical members and to examine the kinematics of the flapping motion, the flapping motion of the system was captured using high-speed video.. The aerodynamic drag forces generated by the prototype were measured based on the captured flapping kinematics. The observations made should benefit in future development of flapping wing vehicles capable of sustained flight.
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spelling ntu-10356/502872023-03-04T18:42:41Z Flapping-flight (I): development of a DC motor-based resonant flapping mechanism for large wing strokes Muhammad Hazwan Ismail. School of Mechanical and Aerospace Engineering Robotics Research Centre Domenico Campolo DRNTU::Engineering::Mechanical engineering This study addresses quantifying the performance of an insect-inspired flapping wing prototype under vacuum condition. The flapping motion was produced by using a single electric motor. Instead of exposing in a vacuum condition, the wings of the flapping prototype were replaced by a pair of rigid cylindrical members that give comparable inertia yet with negligible drag force or aerodynamic damping to achieve the equivalent vacuum environment. For both of the setups, with wings and cylindrical members and to examine the kinematics of the flapping motion, the flapping motion of the system was captured using high-speed video.. The aerodynamic drag forces generated by the prototype were measured based on the captured flapping kinematics. The observations made should benefit in future development of flapping wing vehicles capable of sustained flight. Bachelor of Engineering (Mechanical Engineering) 2012-05-31T06:15:45Z 2012-05-31T06:15:45Z 2012 2012 Final Year Project (FYP) http://hdl.handle.net/10356/50287 en Nanyang Technological University 56 p. application/pdf
spellingShingle DRNTU::Engineering::Mechanical engineering
Muhammad Hazwan Ismail.
Flapping-flight (I): development of a DC motor-based resonant flapping mechanism for large wing strokes
title Flapping-flight (I): development of a DC motor-based resonant flapping mechanism for large wing strokes
title_full Flapping-flight (I): development of a DC motor-based resonant flapping mechanism for large wing strokes
title_fullStr Flapping-flight (I): development of a DC motor-based resonant flapping mechanism for large wing strokes
title_full_unstemmed Flapping-flight (I): development of a DC motor-based resonant flapping mechanism for large wing strokes
title_short Flapping-flight (I): development of a DC motor-based resonant flapping mechanism for large wing strokes
title_sort flapping flight i development of a dc motor based resonant flapping mechanism for large wing strokes
topic DRNTU::Engineering::Mechanical engineering
url http://hdl.handle.net/10356/50287
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