Design of an MAV for the 2019 SAE Aero Design Competition
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open in viewerThe goal of this project was to design a Fixed-Wing Micro Aerial Vehicle in compliance with the rules of the Society of Automotive Engineers 2019 Aero Design Competition. These rules included carrying a payload of 2 inch inner diameter PVC pipe, fitting the unassembled aircraft within a box of dimensions 12.125" x 3.625"x 13.875", and assembling the aircraft in under 3 minutes. The project team conducted analysis and testing in the areas of aircraft structures, stability and controls, aerodynamics, and propulsion. The final aircraft was constructed with laser-cut plywood and balsa, monokote, carbon fiber, and 3D printed components, weighed 2 pounds unloaded and 3.85 pounds loaded, while still meeting all competition requirements.
- This report represents the work of one or more WPI undergraduate students submitted to the faculty as evidence of completion of a degree requirement. WPI routinely publishes these reports on its website without editorial or peer review.
- Creator
- Publisher
- Identifier
- E-project-042119-113102
- Advisor
- Year
- 2019
- Date created
- 2019-04-21
- Resource type
- Major
- Rights statement
关系
- 属于 Collection:
项目
单件
缩略图 | 标题 | 公开度 | Embargo Release Date | 行动 |
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Design_of_an_MAV_for_the_2019_SAE_Aero_Design_Competition.pdf | 公开 | 下载 |
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