摘要
研究了有限长圆筒壳与圆板耦合这一常用结构的耦合损耗因子 ,使用格林函数建立了有限长圆筒壳和圆板的耦合损耗因子计算公式 .与传统半无限长圆筒壳计算公式对比 。
A study of the linked cylinder plate structure which is widely used in flying vehicle has been carried out.The formula for calculating the Coupling Loss Factor between finite length cylinder and circle plate is derived by using the Green Function.It is shown from comparing with traditional formula that the result gained by new formula is more reasonable.
出处
《战术导弹技术》
2002年第2期34-37,共4页
Tactical Missile Technology
关键词
有限长圆筒壳
连接
飞行器
耦合损耗因子
统计能量分析
vehicle
finite length cylinder
circle plate
Coupling Loss Factor(CLF)
Statistical Energy Analysis(SEA)
