Computational investigation on aerodynamic and stability characteristics of a vertical take-off and landing micro air vehicle
This research focuses on the numerical investigation of the aerodynamic and stability characteristics of a Vertical Takeoff and Landing (VTOL) Micro Air Vehicle (MAV). The numerical investigation is divided into two parts: statics and dynamics. In the static analysis, the full configuration of the V...
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Format: | Theses and Dissertations |
Language: | English |
Published: |
2009
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Online Access: | https://hdl.handle.net/10356/19014 |
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Institution: | Nanyang Technological University |
Language: | English |