Abstract
The application of advanced composites on the aerocraft structure can significantly reduce the weight, and improve the aerodynamic and flight performances. In this work, optimization design of a composite wing structure of a minitype unmanned aerial vehicle (UAV) is implemented. The parametric finite element model is established using parametric modeling technique for stress and stain analysis. The global optimal solution is guaranteed by the proposed two-step optimization search strategy combing genetic algorithm (GA) and sequential quadratic programming (SQP).
| Original language | English |
|---|---|
| Title of host publication | Advanced Manufacturing Technology |
| Pages | 1532-1536 |
| Number of pages | 5 |
| DOIs | |
| Publication status | Published - 2011 |
| Event | 2010 International Conference on Advances in Materials and Manufacturing Processes, ICAMMP 2010 - Shenzhen, China Duration: 6 Nov 2010 → 8 Nov 2010 |
Publication series
| Name | Advanced Materials Research |
|---|---|
| Volume | 156-157 |
| ISSN (Print) | 1022-6680 |
Conference
| Conference | 2010 International Conference on Advances in Materials and Manufacturing Processes, ICAMMP 2010 |
|---|---|
| Country/Territory | China |
| City | Shenzhen |
| Period | 6/11/10 → 8/11/10 |
Keywords
- Advanced composite material
- Optimization design
- Parametric finite element modeling
- Structure design
Fingerprint
Dive into the research topics of 'Optimization design of composite wing structure of a minitype unmanned aerial vehicle'. Together they form a unique fingerprint.Cite this
Zhang, Y., Xiong, F., Yang, S., & Mei, X. (2011). Optimization design of composite wing structure of a minitype unmanned aerial vehicle. In Advanced Manufacturing Technology (pp. 1532-1536). (Advanced Materials Research; Vol. 156-157). https://doi.org/10.4028/www.scientific.net/AMR.156-157.1532