Mean Stress Effect on Optimal Overload for Crack Mitigation in Aircraft Panels
47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
2006-01-01
Conference paper
Electronic Resource
English
AIAA-2006-1650 Mean Stress Effect on Optimal Overload for Crack Mitigation in Aircraft Panels
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