The effect of multiple-elevon deflection on the aerodynamic and moment coefficient of a tail-less BWB / Muhammad Aiman Ahmad
The study on BWB UAV begins in UiTM in 2005, focused on the design and fundamental aerodynamics and flight dynamics of small Blended Wing-Body (BWB). The objective of this research was to measure the aerodynamic characteristics on BWB Baseline 7 aircraft. It also to analyse pitching, rolling, and ya...
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| Format: | Thesis |
| Language: | English |
| Published: |
2019
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| Online Access: | https://ir.uitm.edu.my/id/eprint/87856/1/87856.pdf https://ir.uitm.edu.my/id/eprint/87856/ |
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| Summary: | The study on BWB UAV begins in UiTM in 2005, focused on the design and fundamental aerodynamics and flight dynamics of small Blended Wing-Body (BWB). The objective of this research was to measure the aerodynamic characteristics on BWB Baseline 7 aircraft. It also to analyse pitching, rolling, and yawing moment, on the BWB Baseline 7 due to four elevon configuration. The objective was also to determine the control surface configuration for -30, 0, and +30 deflection angle of control surface. |
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