Misran, Amirul Siddiq (2019) Vertical Takeoff And Landing (VTOL) aircraft concept design in supporting medical supply delivery to obsolete area. Project Report. Universiti Teknikal Malaysia Melaka, Melaka, Malaysia. (Submitted)
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Abstract
Vertical take-off and landing application been suggested as the most current flight characteristic to be implemented to the fix wing aircraft. This configuration also affecting the development of small unmanned aerial vehicle as the implementation of this new technology could offer wide range of possibilities. A fix wing SUAV that capable of practicing VTOL can be used as an aerial platform for various application. Performing smooth transition from vertical flight to forward flight, able it to be listed as the most efficient VTOL type of aircraft. It is because VTOL method have been use for aerial vehicle for quite a longtime since the aviation exist in this world, but most of it were from the helicopter type. To make this application integrated to a fix wing aircraft is the current challenge to the engineer based on the idea to develop a fix wing aircraft that can takeoff and landing vertically without runaway while still capable to cruise and glide like an airplane.
Item Type: | Final Year Project (Project Report) |
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Uncontrolled Keywords: | Vertically rising aircraft, Short take-off and landing aircraft, Drone aircraft |
Subjects: | T Technology > T Technology (General) T Technology > TL Motor vehicles. Aeronautics. Astronautics |
Divisions: | Library > Final Year Project > FTKMP |
Depositing User: | Sabariah Ismail |
Date Deposited: | 08 Apr 2021 03:14 |
Last Modified: | 02 Aug 2024 03:27 |
URI: | http://digitalcollection.utem.edu.my/id/eprint/25147 |
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