Micro air vehicles : flapping wing propulsion

This Final Year Report (FYP) investigated the aerodynamic effects of a flapping wing. A water tunnel facility was used in the experiments, testing the effects of a wing in heaving motion on a constant, steady flow. The wing used was a straight wing of airfoil NACA 0012. Two different methods were us...

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Bibliographic Details
Main Author:	Koay, Say Seng.
Other Authors:	Jorg Uwe Schluter
Format:	Final Year Project
Language:	English
Published:	2011
Subjects:	DRNTU::Engineering::Aeronautical engineering::Aircraft
Online Access:	http://hdl.handle.net/10356/45669
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Institution:	Nanyang Technological University
Language:	English

id	sg-ntu-dr.10356-45669
record_format	dspace
spelling	sg-ntu-dr.10356-456692023-03-04T18:45:46Z Micro air vehicles : flapping wing propulsion Koay, Say Seng. Jorg Uwe Schluter School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering::Aircraft This Final Year Report (FYP) investigated the aerodynamic effects of a flapping wing. A water tunnel facility was used in the experiments, testing the effects of a wing in heaving motion on a constant, steady flow. The wing used was a straight wing of airfoil NACA 0012. Two different methods were used separately in the experiments, namely using a pitot static tube and using constant wire anemometry. Bachelor of Engineering (Aerospace Engineering) 2011-06-16T01:59:31Z 2011-06-16T01:59:31Z 2011 2011 Final Year Project (FYP) http://hdl.handle.net/10356/45669 en Nanyang Technological University 58 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::Aeronautical engineering::Aircraft
spellingShingle	DRNTU::Engineering::Aeronautical engineering::Aircraft Koay, Say Seng. Micro air vehicles : flapping wing propulsion
description	This Final Year Report (FYP) investigated the aerodynamic effects of a flapping wing. A water tunnel facility was used in the experiments, testing the effects of a wing in heaving motion on a constant, steady flow. The wing used was a straight wing of airfoil NACA 0012. Two different methods were used separately in the experiments, namely using a pitot static tube and using constant wire anemometry.
author2	Jorg Uwe Schluter
author_facet	Jorg Uwe Schluter Koay, Say Seng.
format	Final Year Project
author	Koay, Say Seng.
author_sort	Koay, Say Seng.
title	Micro air vehicles : flapping wing propulsion
title_short	Micro air vehicles : flapping wing propulsion
title_full	Micro air vehicles : flapping wing propulsion
title_fullStr	Micro air vehicles : flapping wing propulsion
title_full_unstemmed	Micro air vehicles : flapping wing propulsion
title_sort	micro air vehicles : flapping wing propulsion
publishDate	2011
url	http://hdl.handle.net/10356/45669
_version_	1759857967414378496

Micro air vehicles : flapping wing propulsion

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