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

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.

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Abstract

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…

Item Type: Book Section
Creators:
CreatorsEmail
Mohd Ali, ZurriatiUNSPECIFIED
Subjects: L Education > LB Theory and practice of education > Higher Education > Dissertations, Academic. Preparation of theses > Malaysia
Divisions: Institut Pengajian Siswazah (IPSis) : Institute of Graduate Studies (IGS)
Series Name: IGS Biannual Publication
Volume: 8
Number: 8
Item ID: 19597
Uncontrolled Keywords: Abstract; Abstract of thesis; Newsletter; Research information; Doctoral graduates; IPSis; IGS; UiTM; aerodynamics
Last Modified: 07 Jun 2018 02:18
Depositing User: Staf Pendigitalan 5
URI: http://ir.uitm.edu.my/id/eprint/19597

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