摘要
某型飞机机翼挂装翼尖导弹对机翼结构设计和结构分析提出了诸多全新课题 ,如结构的振动响应和气动弹性动响应。
Aircraft with wing-tip missile bring us many new difficulties of structural design and structural analysis such as structural dynamic response analysis and dynamic aeroelastic analysis. This paper presents aircraft discrete gust response analysis.
出处
《飞机设计》
2004年第2期11-18,共8页
Aircraft Design
