摘要
本文介绍一种面向工程实际的复合材料旋翼结构优化设计基本模型,详细阐述了典型剖面、剖面结构形状及自变量的选取。同时还简单介绍了复合材料旋翼桨叶剖面特性分析方法和动力特性分析方法。
This paper introduces a basic composite rotor structural optimization design model for engineering,and details the ways of choosing the typical section locations in span and its section structure shape and the basic parameters in the optimization model.The composite rotor section structure characteristics analysis method and the dynamics characteristics analysis method in the model are introduced briefly too.
出处
《直升机技术》
2009年第2期39-43,共5页
Helicopter Technique
关键词
复合材料
旋翼
结构优化设计模型
composite
rotor
structural optimization design model
