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Subjects
Aluminum alloys, Fatigue, Crack propagationShowing 1 featured edition. View all 1 editions?
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The effect of fatigue crack length on the residual strength of ARALL3 panels with fingertip doublers
1994, National Aerospace Laboratory
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Edition Notes
Bibliographical references: p. 22.
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- Created October 20, 2008
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December 15, 2009 | Edited by WorkBot | link works |
October 20, 2008 | Created by ImportBot | Imported from University of Toronto MARC record |