Longitudinal flight dynamics and stability of blended wing-body unmanned aerial vehicle with canard as control surface / Rizal Effendy Mohd Nasir
Blended wing-body (BWB) aircraft concept has its body ‘blended’ with the wing in smooth transition. Unlike conventional aircraft design, BWB aircraft’s body produces lift force and this causes large impact on the flight dynamics and stability. This thesis focuses on flight dynamics of a small unmann...
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| Format: | Thesis |
| Language: | English |
| Published: |
2013
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| Online Access: | https://ir.uitm.edu.my/id/eprint/16486/6/16486.pdf |
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