Computational fluid dynamic (CFD) analysis of blended wing body (BWB) Baseline-II unmanned aerial vehicle (UAV) with canard setting angle of 10° at 0.1mach number / Nik Ahmad Khalil Badiruddeen
This study investigates the effect of canard on the aerodynamic characteristics of MARA University of Technology's (UiTM) Blended Wing Body (BWB) Baseline-II of Unmanned Aerial Vehicle (UAV) aircraft design. Canard is a small lifting wing located in front of the main wing which is used to impro...
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| Format: | Thesis |
| Language: | English |
| Published: |
2010
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| Subjects: | |
| Online Access: | https://ir.uitm.edu.my/id/eprint/67306/1/67306.pdf |
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