摘要
为解决飞行器尾翼复合材料结构建模复杂、优化工况繁琐等问题,利用Hyper Mesh二次开发技术开发尾翼复合材料建模优化分析系统.介绍该系统相关二次开发技术以及复合材料建模优化分析技术,并给出应用实例.通过该系统可自动建模,自动提交多阶段优化求解和出具结果报告,极大提高尾翼复合材料建模优化分析效率.
To solve the problems of complex structure modeling and complicated optimization eases of aircraft empennage composite, all empennage composite modeling and optimization analysis system is developed using the HyperMesh secondal7 development technique. An application example is given to introduce the relevant secondary development technique and composite modeling and optimization analysis technique. The automatic modeling, muti-stage job by the system. It also greatly improve the efficiency composite. submission and result reporting can be implemented of modeling and optimization analysis of empennage
出处
《计算机辅助工程》
2016年第3期29-33,共5页
Computer Aided Engineering
关键词
飞行器
尾翼
复合材料优化
自由尺寸优化
铺层优化
自动建模
TCL/TK
aircraft
empennage
composite optimization
fi＇ee size optimization
shuffling optimization
automatic modeling
Tcl/Tk
