Title of article :
Fatigue failure of adhesively patched 2024-T3 and 7075-T6 clad and bare aluminium alloys
Author/Authors :
D. L. DUQUESNAY، نويسنده , , P. R. UNDERHILL، نويسنده , , H. J. BRITT، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2005
Keywords :
adhesive • aircraft • aluminium • cladding • corrosion • damage • fatigue • patch • repair
Journal title :
Fatigue and Fracture of Engineering Materials and Structures
Journal title :
Fatigue and Fracture of Engineering Materials and Structures