Aeroelasticity and Dynamic Analysis of Cracked Composite Wings Using Spectral Finite Element Method (AIAA 2014-0677)
Conference; 55th, AIAA/ASME/ASME/ASCE/AHS/SC Structures, structural dynamics and materials ; 2014 ; National Harbor, MD
2014-01-01
13 pages
Includes bibliographical references and author index
Conference paper
English
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