摘要
CFRP增强铝合金梁结构中,两种材料之间的载荷传递主要是通过界面胶结层的变形来实现的。本文主要针对该结构中界面应力进行理论计算,并且对其影响因素进行讨论分析。
In the structure of CFRP reinforced aluminum alloy beam, the load between the two kinds of materials, transfer mainly through the deformation of the interface cement layer. This discourse mainly calculates the interfacial stress in the structure from theory, and makes discussion and analysis of its influencing factors.
出处
《飞机设计》
2010年第3期45-47,80,共4页
Aircraft Design
关键词
CFRP
界面剪应力
界面剥离应力
CFRP
interface shear stress
interface debonding stress
