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

Rashid, Rohayati Ab (2011) Experimental Study On The Wing Structure And Skin Flexibility For Flapping Wing Of Micro Aerial Vehicle (MAV). Masters thesis, Universiti Sains Malaysia.

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Abstract

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.

Item Type:	Thesis (Masters)
Subjects:	T Technology > TJ Mechanical engineering and machinery > TJ1 Mechanical engineering and machinery
Divisions:	Kampus Kejuruteraan (Engineering Campus) > Pusat Pengajian Kejuruteraan Mekanikal (School of Mechanical Engineering) > Thesis
Depositing User:	ASM Ab Shukor Mustapa
Date Deposited:	12 Oct 2018 02:19
Last Modified:	12 Apr 2019 05:26
URI:	http://eprints.usm.my/id/eprint/42449

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