THE FLUTTER MODEL CHARACTERISTIC STUDY AND WIND-TUNNEL TEST FOR WING-MOUNTED CIVIL AIRCRAFT

摘要：

　　The body-like aerodynamic model are used for the fuselage and nacelle component.The influence of the flutter characteristic due to aerodynamic of the fuselage and nacelle are studied and verified through low-speed flutter model wind-tunnel test of the aircraft.The theoretical results and test results show that the flutter characteristic of the aircraft is changed considering aerodynamic effect of fuselage and nacelle.

关键词： wing-mounted civil aircraft body-like aerodynamic model flutter aeroelasticity

作者: Chen Lei Dou Zhongqian

作者单位: Stress Department,Shanghai Aircraft Design and Research Institute,Commercial Aircraft Corporation of China,Shanghai 201210

会议类型: 国内会议

会议名称: 第十四届全国空气弹性学术交流会

会议地点: 西安

会议语种:英文

页码: 1-8

在线出版日期: 2015-08-01（万方平台首次上网日期，不代表论文的发表时间）