Design Flight Tests Small Flying is a M.Tech project topic for Aerospace Engineering. It gives students a clear starting point for research, implementation planning, and documentation.
Design Flight Tests Small Flying Project Details
| Abstract |
This study focuses on the design and the flight tests of a new small unmanned aerial vehicle (UAV) with a flying wing design. The design exploits the benefits of a flying wing such as lower aerodynamic drag making it more suitable for long endurance missions including observation, surveillance, and search and rescue missions. The design approach attempts to achieve stability without the use of vertical stabilizers or other artificial stabilization systems, which could reduce aerodynamic efficiency. The project includes elaborated design and analysis to achieve the necessary stability in both static and dynamic aerodynamic performance. Flight tests are designed to demonstrate the functionality and stability of the configuration under various
conditions. The results illustrate that a flying wing UAV has been developed that can achieve stable flight without the use of artificial stabilization. The study illustrates the need for extensive research on this type of configuration for small unmanned aerial vehicles, especially for missions that require high endurance, low energy consumption and low detection capabilities.
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| Reference Paper |
Design and Flight Tests of a Small Flying Wing UAV |
| Domain |
Aerospace Engineering |
| Sub-Domain |
Structures & Systems / Guidance Navigation Control / Autopilot Design |
| PDF Download |
Download / View PDF |
| Get Help |
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