Residual strength prediction of aircraft fuselages using crack-tip opening angle criterion
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2011 ◽
Vol 172
(1)
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pp. 105-112
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2008 ◽
Vol 75
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pp. 3599-3610
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pp. 2091-2099
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pp. 187-195
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2003 ◽
Vol 70
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pp. 443-456
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2021 ◽
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