基于Aerobook的翼身融合复合材料飞机结构优化与强度校核

Composite BWB Aircraft Structure Optimization and Verification by Aerobook Software Platform

复合材料飞机机体结构强度优化设计自由度大,强度设计要求高;基于Aerobook软件平台,对一复合材料翼身融合飞机进行了布局方案模型构建,以及优化和校核;为复合材料飞机结构的布局、尺寸优化设计和快速迭代提供了可行的解决方案。

Composite aircraft structure strength optimization is with design freedom,strength design requirements;The composite blended wing body(BWB) aircraft layout sizing was optimized and verified by Aerobook software platform.The Aerobook software platform get the solution for the composite structure optimization design and rapid sizing.