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Design and Optimization of Wing Structure for a Fixed-Wing Unmanned Aerial Vehicle (UAV)
| Content Provider | Semantic Scholar |
|---|---|
| Author | Yu, Jiawen |
| Copyright Year | 2018 |
| Abstract | The wing, one of the most important parts of aircraft, always requires sophis-ticated design to increase lift, reduce drag and weight. For modern fixed-wing UAV, extending cruising time is always a requirement for the overall design. Designing a most light wing that can match the requirements of work condi-tions is desired. In this work, according to the work conditions, we compare several types of wing and chose beam-type wing. Then we made the detailed design and optimization to reduce the weight of wing. At last, we draw the 3D model for potential realistic production. |
| Starting Page | 249 |
| Ending Page | 263 |
| Page Count | 15 |
| File Format | PDF HTM / HTML |
| DOI | 10.4236/mme.2018.84017 |
| Volume Number | 08 |
| Alternate Webpage(s) | https://file.scirp.org/pdf/MME_2018112014591314.pdf |
| Alternate Webpage(s) | https://doi.org/10.4236/mme.2018.84017 |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |
