Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV)

Micro Aerial Vehicle (MAV) in Malaysia is still at an early stage. Therefore, the development of flapping a wing MAV by Aerodynamic Laboratory in School of Mechanical Universiti Sains Malaysia, encourage the local researchers and scientist to study the importance and the capability of flapping a win...

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Main Author:	Rashid, Rohayati Ab
Format:	Thesis
Language:	English
Published:	2011
Subjects:	TJ1 Mechanical engineering and machinery
Online Access:	http://eprints.usm.my/42449/1/ROHAYATI_AB_RASHID.pdf
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id	my-usm-ep.42449
record_format	uketd_dc
spelling	my-usm-ep.424492019-04-12T05:26:37Z Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV) 2011-05 Rashid, Rohayati Ab TJ1 Mechanical engineering and machinery Micro Aerial Vehicle (MAV) in Malaysia is still at an early stage. Therefore, the development of flapping a wing MAV by Aerodynamic Laboratory in School of Mechanical Universiti Sains Malaysia, encourage the local researchers and scientist to study the importance and the capability of flapping a wing MAV. The flapping wing MAV shows great promise in civilian and military applications as it possesses good maneuverability at low speeds and relatively good energy efficiency. Hence, it is vital for the MAV to be able to carry a certain load of additional equipment in accordance to performing its function successfully. 2011-05 Thesis http://eprints.usm.my/42449/ http://eprints.usm.my/42449/1/ROHAYATI_AB_RASHID.pdf application/pdf en public masters Universiti Sains Malaysia Pusat Pengajian Kejuteraan Makanikal
institution	Universiti Sains Malaysia
collection	USM Institutional Repository
language	English
topic	TJ1 Mechanical engineering and machinery
spellingShingle	TJ1 Mechanical engineering and machinery Rashid, Rohayati Ab Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV)
description	Micro Aerial Vehicle (MAV) in Malaysia is still at an early stage. Therefore, the development of flapping a wing MAV by Aerodynamic Laboratory in School of Mechanical Universiti Sains Malaysia, encourage the local researchers and scientist to study the importance and the capability of flapping a wing MAV. The flapping wing MAV shows great promise in civilian and military applications as it possesses good maneuverability at low speeds and relatively good energy efficiency. Hence, it is vital for the MAV to be able to carry a certain load of additional equipment in accordance to performing its function successfully.
format	Thesis
qualification_level	Master's degree
author	Rashid, Rohayati Ab
author_facet	Rashid, Rohayati Ab
author_sort	Rashid, Rohayati Ab
title	Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV)
title_short	Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV)
title_full	Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV)
title_fullStr	Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV)
title_full_unstemmed	Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV)
title_sort	experimental study on the wing structure and skin flexibility for flapping wing of micro aerial vehicle (mav)
granting_institution	Universiti Sains Malaysia
granting_department	Pusat Pengajian Kejuteraan Makanikal
publishDate	2011
url	http://eprints.usm.my/42449/1/ROHAYATI_AB_RASHID.pdf
_version_	1747821069226475520

Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV)

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