摘要
为研制先进的导弹弹翼，用新研制的复合材料制成工字梁，模拟导弹飞行时翼梁受热弯条件进行实验，测出梁的温度和挠度随时间变化曲线，确定正常使用条件和失效形式．用此复合材料代替现役导弹的金属材料，可明显减重。
The experimental investigation of the bending of C/K composite beams at transient high temperature,was presented.The conductive temperature distribution and the bending deflection curves of the composite beams were obtained.It shows that the damage form of the bending specimens is buckling.
出处
《北京航空航天大学学报》
EI
CAS
CSCD
北大核心
1996年第3期385-388,共4页
Journal of Beijing University of Aeronautics and Astronautics
