2 . a new structural optimization algorithm combined with the half-determined ga and the hybrid approximation techniques is proposed 利用混合近似技術和對偶理論,建立了一般的基于遺傳算法的結構優(yōu)化設計的框架。
In this dissertation, we combined the knowledge of paralleled algorithm, networks, fem, structural optimization algorithm and others correlative fields, improved and realized a distributed paralleled optimization system with separate module based on corba 作者結合并行算法、分布式計算、計算機網(wǎng)絡、有限元分析方法,結構優(yōu)化算法和其他相關學科,改進并開發(fā)出基于corba的分布式并行優(yōu)化系統(tǒng),該系統(tǒng)具有獨立的基于corba的分布式并行計算模塊。
Combined with modem structural finite element analysis, modern structural optimization algorithms, composite structures mechanics and aeroelastic tailoring of composite wing as well as relative high performance numerical method, a system named the composite synthesis optimization for aircraft structures ( cosoas ), has been developed in this paper, which has own independent component of finite element analysis 本文結合現(xiàn)代結構有限元分析方法、現(xiàn)代結構優(yōu)化算法、復合材料結構力學、復合材料氣動彈性剪裁設計方法以及相關的高性能數(shù)值計算工具開發(fā)出了擁有自己獨立有限元程序的復合材料飛機結構綜合優(yōu)化設計系統(tǒng)(cosoas)。在內容上本文突出復合材料應用特色。
The distributed structural optimization computing system has been designed and developed on the basis of the distributed computation, the distributed object technology, the computer network, the finite element analysis method, the structural optimization algorithm and other correlation subject researches 分布式的結構優(yōu)化計算系統(tǒng)是在作者結合分布式計算、分布式對象技術、計算機網(wǎng)絡、有限元分析方法、結構優(yōu)化算法以及其他相關學科研究的基礎上設計并開發(fā)出來的。