Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali

The Blended Wing-Body (BWB) aircraft is an unconventional aircraft that offers the aerodynamics performance advantages compared to the conventional aircraft. This type of aircraft has a unique design where the main body is blended together with the wing that gives the additional lift of the aircraft...

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Main Author: Mohd Ali, Zurriati
Format: Book Section
Language:English
Published: Institute of Graduate Studies, UiTM 2015
Subjects:
Online Access:https://ir.uitm.edu.my/id/eprint/19597/
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author Mohd Ali, Zurriati
author_facet Mohd Ali, Zurriati
author_sort Mohd Ali, Zurriati
building UiTM Institutional Repository
collection Online Access
description The Blended Wing-Body (BWB) aircraft is an unconventional aircraft that offers the aerodynamics performance advantages compared to the conventional aircraft. This type of aircraft has a unique design where the main body is blended together with the wing that gives the additional lift of the aircraft. In contrast to the conventional aircraft, the BWB has a poor stability due to the absence of the tail. A possible solution is by using a horizontal control surface, the canard, to improve the stability of the BWB. For this purpose, a comprehensive investigation of the aerodynamic behavior of the BWB with canard is important…
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institution Universiti Teknologi MARA
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language English
last_indexed 2025-11-14T22:01:03Z
publishDate 2015
publisher Institute of Graduate Studies, UiTM
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spelling uitm-195972018-06-07T02:18:42Z https://ir.uitm.edu.my/id/eprint/19597/ Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali Mohd Ali, Zurriati Malaysia The Blended Wing-Body (BWB) aircraft is an unconventional aircraft that offers the aerodynamics performance advantages compared to the conventional aircraft. This type of aircraft has a unique design where the main body is blended together with the wing that gives the additional lift of the aircraft. In contrast to the conventional aircraft, the BWB has a poor stability due to the absence of the tail. A possible solution is by using a horizontal control surface, the canard, to improve the stability of the BWB. For this purpose, a comprehensive investigation of the aerodynamic behavior of the BWB with canard is important… Institute of Graduate Studies, UiTM 2015 Book Section PeerReviewed text en https://ir.uitm.edu.my/id/eprint/19597/1/ABS_ZURRIATI%20MOHD%20ALI%20TDRA%20VOL%208%20IGS%2015.pdf Mohd Ali, Zurriati (2015) Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali. (2015) In: The Doctoral Research Abstracts. IGS Biannual Publication, 8 (8). Institute of Graduate Studies, UiTM, Shah Alam.
spellingShingle Malaysia
Mohd Ali, Zurriati
Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali
title Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali
title_full Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali
title_fullStr Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali
title_full_unstemmed Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali
title_short Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali
title_sort effects of canard configuration on the aerodynamics of blended wing body at low mach number / zurriati mohd ali
topic Malaysia
url https://ir.uitm.edu.my/id/eprint/19597/