Two Stage Damage Tolerance Evaluation of an Aircraft Fuselage Panel with a Circumferential Crack and a Broken Stringer
Conference; 54th, Structures, structural dynamics and materials; 54th AIAA/ASME/ASCE/AHS/ASC structures ; 2013 ; Boston, MA
2013-01-01
20 pages
Includes bibliographical references and index
Conference paper
English
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