The effect of tail sweep angle to the aerodynamics and stability of a blended wing body aircraft (baseline V) / Mohamad Zulfazli Arief Abd Latif

Blended wing body (BWB) aircraft is theoretically designed based on the combination of conventional aircraft and flying wing which is likely to be the future concept of an aircraft. Some of the studies claim that BWB aircraft has higher lift to drag ratio compared to the conventional aircraft. Howev...

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Main Author:	Abd Latif, Mohamad Zulfazli Arief
Format:	Thesis
Language:	English
Published:	2019
Online Access:	https://ir.uitm.edu.my/id/eprint/87878/1/87878.pdf
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id	my-uitm-ir.87878
record_format	uketd_dc
spelling	my-uitm-ir.878782024-04-18T08:26:26Z The effect of tail sweep angle to the aerodynamics and stability of a blended wing body aircraft (baseline V) / Mohamad Zulfazli Arief Abd Latif 2019 Abd Latif, Mohamad Zulfazli Arief Blended wing body (BWB) aircraft is theoretically designed based on the combination of conventional aircraft and flying wing which is likely to be the future concept of an aircraft. Some of the studies claim that BWB aircraft has higher lift to drag ratio compared to the conventional aircraft. However, by obtaining high lift to drag ratio only does not means that the aircraft has good longitudinal stability. Flight Technology and Test Centre (FTTC), Universiti Teknologi MARA Shah Alam began the research on BWB aircraft in 2005 and found problem related to the stability of the aircraft. Some ideas have been proposed to overcome the BWB‟s poor flight stability such as having large central elevator, installing canard, designing planform that mimics a bird, and installing long tail boom. 2019 Thesis https://ir.uitm.edu.my/id/eprint/87878/ https://ir.uitm.edu.my/id/eprint/87878/1/87878.pdf text en public masters Universiti Teknologi MARA (UiTM) Faculty of Mechanical Engineering Mohd Nasir, Rizal Effendy
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Mohd Nasir, Rizal Effendy
description	Blended wing body (BWB) aircraft is theoretically designed based on the combination of conventional aircraft and flying wing which is likely to be the future concept of an aircraft. Some of the studies claim that BWB aircraft has higher lift to drag ratio compared to the conventional aircraft. However, by obtaining high lift to drag ratio only does not means that the aircraft has good longitudinal stability. Flight Technology and Test Centre (FTTC), Universiti Teknologi MARA Shah Alam began the research on BWB aircraft in 2005 and found problem related to the stability of the aircraft. Some ideas have been proposed to overcome the BWB‟s poor flight stability such as having large central elevator, installing canard, designing planform that mimics a bird, and installing long tail boom.
format	Thesis
qualification_level	Master's degree
author	Abd Latif, Mohamad Zulfazli Arief
spellingShingle	Abd Latif, Mohamad Zulfazli Arief The effect of tail sweep angle to the aerodynamics and stability of a blended wing body aircraft (baseline V) / Mohamad Zulfazli Arief Abd Latif
author_facet	Abd Latif, Mohamad Zulfazli Arief
author_sort	Abd Latif, Mohamad Zulfazli Arief
title	The effect of tail sweep angle to the aerodynamics and stability of a blended wing body aircraft (baseline V) / Mohamad Zulfazli Arief Abd Latif
title_short	The effect of tail sweep angle to the aerodynamics and stability of a blended wing body aircraft (baseline V) / Mohamad Zulfazli Arief Abd Latif
title_full	The effect of tail sweep angle to the aerodynamics and stability of a blended wing body aircraft (baseline V) / Mohamad Zulfazli Arief Abd Latif
title_fullStr	The effect of tail sweep angle to the aerodynamics and stability of a blended wing body aircraft (baseline V) / Mohamad Zulfazli Arief Abd Latif
title_full_unstemmed	The effect of tail sweep angle to the aerodynamics and stability of a blended wing body aircraft (baseline V) / Mohamad Zulfazli Arief Abd Latif
title_sort	effect of tail sweep angle to the aerodynamics and stability of a blended wing body aircraft (baseline v) / mohamad zulfazli arief abd latif
granting_institution	Universiti Teknologi MARA (UiTM)
granting_department	Faculty of Mechanical Engineering
publishDate	2019
url	https://ir.uitm.edu.my/id/eprint/87878/1/87878.pdf
_version_	1804889794296152064

The effect of tail sweep angle to the aerodynamics and stability of a blended wing body aircraft (baseline V) / Mohamad Zulfazli Arief Abd Latif

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