孙宏涛.复合材料胶接修补止裂技术的理论及试验研究[D].西安:西北工业大学博士论文,1998.[5] BAKER A A.Fiber composite repair of cracked metallic aircraft components:practical and basic aspects[J].Composites,1987,18(4):293-307.
[4]
BAKER A A.Reinforcement of the F-111 wing pivot fitting with a born/epoxy doubler system materials engineering aspects[J].Composites,1993,24(6):511-521.
LUNDER O,OLSEN B,NISANCIOGLU.Pre-treatment of AA6060 aluminum alloy for adhesive bonding[J].International Journal of Adhesion & Adhesives,2002,22:143-150.
[13]
ASTRID B,FABRICE L,JOHN W.Anodising as pre-treatment for structural bonding[J].International Journal of Adhesion & Adhesives 2003,23:401-412.
[14]
OSBORNE J H,BLOHOWIAK K Y,TAYLOR S R,et al.Testing and evaluation of nonchromated coating systems for aerospace applications[J].Progress in Organic Coatings 2001,41:217-225.
[15]
ASTM D 1002-01,Standard Test Method for Apparent Shear Strength of Single-Lap-Joint Adhesively Bonded Metal Specimens by Tension Loading (Metal-to-Metal)[S].Pennsylvania,USA:Annual Book of ASTM Standards,2001.
[16]
陈篪,蔡其巩,王仁智,等.工程断裂力学[M].北京:国防工业出版社,1978.
[17]
WANG Q Y,PIDAPARTI R M.Static characteristics and fatigue behavior of composite repaired aluminum plates[J].Composite Structures,2002,56:151-155.