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: | https://ir.uitm.edu.my/id/eprint/19597/1/ABS_ZURRIATI%20MOHD%20ALI%20TDRA%20VOL%208%20IGS%2015.pdf |
| _version_ | 1825735245520961536 |
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| author | Mohd Ali, Zurriati |
| author_facet | Mohd Ali, Zurriati |
| author_sort | Mohd Ali, Zurriati |
| collection | UITM |
| 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… |
| first_indexed | 2024-03-06T01:44:10Z |
| format | Book Section |
| id | oai:ir.uitm.edu.my:19597 |
| institution | Universiti Teknologi MARA |
| language | English |
| last_indexed | 2024-03-06T01:44:10Z |
| publishDate | 2015 |
| publisher | Institute of Graduate Studies, UiTM |
| record_format | dspace |
| spelling | oai:ir.uitm.edu.my: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 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/19597/1/ABS_ZURRIATI%20MOHD%20ALI%20TDRA%20VOL%208%20IGS%2015.pdf |
| work_keys_str_mv | AT mohdalizurriati effectsofcanardconfigurationontheaerodynamicsofblendedwingbodyatlowmachnumberzurriatimohdali |