Design and analysis of adhesively bonded thick composite patch repair of corrosion grind-out and cracks on 2024 T3 clad aluminum aging aircraft structures
2006 ◽
Vol 76
(1-2)
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pp. 138-150
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2005 ◽
Vol 71
(2)
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pp. 258-270
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2004 ◽
Vol 11
(4)
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pp. 191-203
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1997 ◽
Vol 19
(8-9)
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pp. 660-660
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2015 ◽
Vol 230
(8)
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pp. 1448-1466
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2011 ◽
Vol 42
(3)
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pp. 505-510
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