基于HyperMesh二次开发的飞行器尾翼复合材料建模和优化分析

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HyperMesh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.

Modeling and optimization analysis on aircraft empennage composite based on secondary development of HyperMesh

To solve the problems of complex structure modeling and complicated optimization cases of aircraft empennage composite, an empennage composite modeling and optimization analysis system is developed using the HyperMesh secondary 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 submission and result reporting can be implemented by the system. It also greatly improve the efficiency of modeling and optimization analysis of empennage composite.