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Aerodynamic Performance Optimization Design for Aircraft Based on Improved Genetic Algorithm
| Content Provider | Semantic Scholar |
|---|---|
| Author | Guo, Hongbo |
| Copyright Year | 2017 |
| Abstract | In order to improve the aerodynamic optimization design efficiency and using multi-objective optimization algorithm solving non-inferior solutions sets efficiency, a multi-objective optimization method is developed to solve the multi-objective problem of aerodynamic design for aircraft, and then an optimization algorithm for the aerodynamic system is proposed based on the characteristics of the Pareto method. At last, the integrated optimization design of aerodynamic and stealth characteristics is given. The results show that the aerodynamic performance of the wing is improved by the optimized design, to achieve the purpose of optimization design, and the optimized wing design method is feasible. |
| File Format | PDF HTM / HTML |
| DOI | 10.21311/001.39.10.25 |
| Alternate Webpage(s) | http://tjfeonline.com/admin/archive/2504.01.20171483532138.pdf |
| Alternate Webpage(s) | https://doi.org/10.21311/001.39.10.25 |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |