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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| Format: | Book Section |
| Language: | English |
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Institute of Graduate Studies, UiTM
2015
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| 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 |
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uitm-19597 |
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eprints |
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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 |
| _version_ |
1777418292134150144 |