摘要
为提高飞机蒙皮裂纹的修补效能 ,通过优选材料合理地确定修补参数 ,有效地降低了裂纹附近的应力强度因子 。
In order to increase the efficacy of repair for the cracks on aluminum alloy skin of aircraft,through the optimum of materials the repair parameters were determined.So that the intensive factor of the stress by craks was effectively decreased and the serviceable life of the damaged structure was renewed.
出处
《粘接》
CAS
2002年第3期48-49,共2页
Adhesion
