Abstract
Taking sweptwing as example of aerodynamic optimization, integration framework of aerodynamic was built based on Model Center software with VB program, CAD, CFD software and genetic algorithm. Two kinds of optimization projects, Multi-objective Genetic Algorithm associate with three-dimensional CFD and response surface models (RSM) respectively, were used in the optimization process. The result of two projects associating with analysis of flow field demonstrates feasibility and robustness of those projects for aerodynamic optimization design and integration framework.
| Original language | English |
|---|---|
| Pages (from-to) | 1033-1036+1039 |
| Journal | Xitong Fangzhen Xuebao / Journal of System Simulation |
| Volume | 21 |
| Issue number | 4 |
| Publication status | Published - 20 Feb 2009 |
Keywords
- CFD
- Genetic algorithm
- Integration framework
- Multi-objective aerodynamic optimization design
- RSM
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Meng, L. T., Liu, L., Long, T., & Zhu, H. G. (2009). Multi-objective aerodynamic optimization of sweptwing. Xitong Fangzhen Xuebao / Journal of System Simulation, 21(4), 1033-1036+1039.