机翼前缘及气动弹性优化设计研究进展  

Research Progress of Leading Edge and Aeroelasticity Optimization Design

作　　者：秦琴[1] 李立强 易清洋 邵云峰 Qin Qin;Li Liqiang;Yi Qingyang;Shao Yunfeng(Institute of Intelligent Manufacturing, Jincheng College, Sichuan University, Chengdu 611731, China)

机构地区：[1]四川大学锦城学院智能制造学院,成都611731

出　　处：《黑龙江科学》2021年第16期25-26,29,共3页Heilongjiang Science

摘　　要：以飞机机翼为研究对象,总结了机翼固定前缘的设计现状,从机动载荷、复合材料机翼壁板、铺层比例三方面综述机翼气动弹性研究进展,给出了机翼优化设计建议。Through taking aircraft wing as the research objects,the research summarizes the design status of aircraft wing fixed leading edge,and research progress of leading edge aeroelasticity from the following three aspects,including maneuvering load,composite wing wall and lay up ratio.Then the research proposes the design suggestion for aerofoil optimization.

关 键 词：机翼 固定前缘 气动弹性设计 机动载荷 铺层比例 

分 类 号：TB331[一般工业技术—材料科学与工程]