Development of a multi-rotor VTOL UAV : computation of aerodynamics forces and moments using CFD
A VTOL model aircraft is analysed using CFD code. The model was first conceptually designed using a simplified design code XFLR5, and a full detailed assessment of the model is performed. Detailed mesh independence studies were performed and the results for longitudinal motion were obtained. Furt...
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| Format: | Final Year Project (FYP) |
| Language: | English |
| Published: |
2018
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| Online Access: | http://hdl.handle.net/10356/75581 |