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.
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 Details
| Item Type: | Book Section |
|---|---|
| Creators: | Creators Email / ID Num. Mohd Ali, Zurriati UNSPECIFIED |
| Subjects: | L Education > LB Theory and practice of education > Higher Education > Dissertations, Academic. Preparation of theses > Malaysia |
| Divisions: | Universiti Teknologi MARA, Shah Alam > Institut Pengajian Siswazah (IPSis) : Institute of Graduate Studies (IGS) |
| Series Name: | IGS Biannual Publication |
| Volume: | 8 |
| Number: | 8 |
| Keywords: | Abstract; Abstract of thesis; Newsletter; Research information; Doctoral graduates; IPSis; IGS; UiTM; aerodynamics |
| Date: | 2015 |
| URI: | https://ir.uitm.edu.my/id/eprint/19597 |
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