The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software

In line with the advancement of micro processor technology, availability small scale aircraft engine model, light weight material and also better understanding in the aircraft design process had brought a current attention to develop autonomous flying vehicles. This kind of vehicle has offered v...

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Main Author:	Al Aian, Ahmad Eshtiwey
Format:	Thesis
Language:	English English English
Published:	2011
Subjects:	TL Motor vehicles Aeronautics Astronautics
Online Access:	http://eprints.uthm.edu.my/2583/1/24p%20AHMAD%20ESHTIWEY%20AL%20AIAN.pdf http://eprints.uthm.edu.my/2583/2/AHMAD%20ESHTIWEY%20AL%20AIAN%20COPYRIGHT%20DECLARATION.pdf http://eprints.uthm.edu.my/2583/3/AHMAD%20ESHTIWEY%20AL%20AIAN%20WATERMARK.pdf
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id	my-uthm-ep.2583
record_format	uketd_dc
spelling	my-uthm-ep.25832021-11-01T02:46:07Z The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software 2011-12 Al Aian, Ahmad Eshtiwey TL Motor vehicles. Aeronautics. Astronautics TL500-777 Aeronautics. Aeronautical engineering In line with the advancement of micro processor technology, availability small scale aircraft engine model, light weight material and also better understanding in the aircraft design process had brought a current attention to develop autonomous flying vehicles. This kind of vehicle has offered various applications, such as military and civilian purposes. However to develop such kind autonomous flying vehicles one have to develop a control law which govern how the flying vehicle to fly. To do so one have to prepare firstly the required aerodynamics data. The present work focused on the type of flying vehicle powered by electric type of engine. This type of engine is normally available in the market is at the size of engine less than 5 hp. Due to the engine limitation, the size of flying vehicle. has been decided to the aircraft configuration with all required devices for autonomous they vehicle is no more than 6 Kg. through series of aerodynamics assessment aircraft components (fuselage, wing, airfoil on the control surface and it's high lift devices). the present special write produce an initial aircraft configuration with aerodynamic data which can be future studied for development that aircraft as an autonomous flying vehicle. 2011-12 Thesis http://eprints.uthm.edu.my/2583/ http://eprints.uthm.edu.my/2583/1/24p%20AHMAD%20ESHTIWEY%20AL%20AIAN.pdf text en public http://eprints.uthm.edu.my/2583/2/AHMAD%20ESHTIWEY%20AL%20AIAN%20COPYRIGHT%20DECLARATION.pdf text en staffonly http://eprints.uthm.edu.my/2583/3/AHMAD%20ESHTIWEY%20AL%20AIAN%20WATERMARK.pdf text en validuser mphil masters Universiti Tun Hussein Malaysia Fakulti Kejuruteraan Mekanikal dan Pembuatan
institution	Universiti Tun Hussein Onn Malaysia
collection	UTHM Institutional Repository
language	English English English
topic	TL Motor vehicles Aeronautics Astronautics TL Motor vehicles Aeronautics Astronautics
spellingShingle	TL Motor vehicles Aeronautics Astronautics TL Motor vehicles Aeronautics Astronautics Al Aian, Ahmad Eshtiwey The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software
description	In line with the advancement of micro processor technology, availability small scale aircraft engine model, light weight material and also better understanding in the aircraft design process had brought a current attention to develop autonomous flying vehicles. This kind of vehicle has offered various applications, such as military and civilian purposes. However to develop such kind autonomous flying vehicles one have to develop a control law which govern how the flying vehicle to fly. To do so one have to prepare firstly the required aerodynamics data. The present work focused on the type of flying vehicle powered by electric type of engine. This type of engine is normally available in the market is at the size of engine less than 5 hp. Due to the engine limitation, the size of flying vehicle. has been decided to the aircraft configuration with all required devices for autonomous they vehicle is no more than 6 Kg. through series of aerodynamics assessment aircraft components (fuselage, wing, airfoil on the control surface and it's high lift devices). the present special write produce an initial aircraft configuration with aerodynamic data which can be future studied for development that aircraft as an autonomous flying vehicle.
format	Thesis
qualification_name	Master of Philosophy (M.Phil.)
qualification_level	Master's degree
author	Al Aian, Ahmad Eshtiwey
author_facet	Al Aian, Ahmad Eshtiwey
author_sort	Al Aian, Ahmad Eshtiwey
title	The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software
title_short	The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software
title_full	The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software
title_fullStr	The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software
title_full_unstemmed	The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software
title_sort	aerodynamics analysis of type uav aircraft with pusher engine configuration by use of datcom software
granting_institution	Universiti Tun Hussein Malaysia
granting_department	Fakulti Kejuruteraan Mekanikal dan Pembuatan
publishDate	2011
url	http://eprints.uthm.edu.my/2583/1/24p%20AHMAD%20ESHTIWEY%20AL%20AIAN.pdf http://eprints.uthm.edu.my/2583/2/AHMAD%20ESHTIWEY%20AL%20AIAN%20COPYRIGHT%20DECLARATION.pdf http://eprints.uthm.edu.my/2583/3/AHMAD%20ESHTIWEY%20AL%20AIAN%20WATERMARK.pdf
_version_	1747830966854877184

The aerodynamics analysis of type UAV aircraft with pusher engine configuration by use of DATCOM software

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