Abstract
A high-efficiency aeroelastic optimization method based on Kriging model and genetic algorithm is presented, and the method is verified by aeroelastic optimization of composite wing. The accuracy of aeroelastic optimization based on Kriging model is analyzed and the framework of aeroelastic optimization base on Kriging model and genetic algorithm is presented. The feasibility of the method is verified by an example, and the effects of design variable number and constraint number on optimization efficiency and result are analyzed in detail.
| Original language | English |
|---|---|
| State | Published - 2015 |
| Event | 16th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2015 - Saint Petersburg, Russian Federation Duration: 28 Jun 2015 → 2 Jul 2015 |
Conference
| Conference | 16th International Forum on Aeroelasticity and Structural Dynamics, IFASD 2015 |
|---|---|
| Country/Territory | Russian Federation |
| City | Saint Petersburg |
| Period | 28/06/15 → 2/07/15 |
Keywords
- Aeroelastic optimization
- Composite wing
- High-efficiency
- Kriging model
Fingerprint
Dive into the research topics of 'A high-efficiency aeroelastic optimization method based on kriging model and genetic algorithm'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver