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:http://ir.uitm.edu.my/id/eprint/19597/
http://ir.uitm.edu.my/id/eprint/19597/1/ABS_ZURRIATI%20MOHD%20ALI%20TDRA%20VOL%208%20IGS%2015.pdf
id uitm-19597
recordtype eprints
spelling uitm-195972018-06-07T02:18:42Z http://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 http://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. In: The Doctoral Research Abstracts. IGS Biannual Publication, 8 (8). Institute of Graduate Studies, UiTM, Shah Alam.
repository_type Digital Repository
institution_category Local University
institution Universiti Teknologi MARA
building UiTM Institutional Repository
collection Online Access
language English
topic Malaysia
spellingShingle Malaysia
Mohd Ali, Zurriati
Effects of canard configuration on the aerodynamics of blended wing body at low mach number / Zurriati Mohd Ali
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…
format Book Section
author Mohd Ali, Zurriati
author_facet Mohd Ali, Zurriati
author_sort Mohd Ali, Zurriati
title 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_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_sort effects of canard configuration on the aerodynamics of blended wing body at low mach number / zurriati mohd ali
publisher Institute of Graduate Studies, UiTM
publishDate 2015
url http://ir.uitm.edu.my/id/eprint/19597/
http://ir.uitm.edu.my/id/eprint/19597/1/ABS_ZURRIATI%20MOHD%20ALI%20TDRA%20VOL%208%20IGS%2015.pdf
first_indexed 2023-09-18T23:02:54Z
last_indexed 2023-09-18T23:02:54Z
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