Buckling behavior of laminated composite stiffened cylindrical shell panels having cutout for different parametric variations
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DOI: 10.1177/09544062221100613
Abstract: Buckling of composite stiffened cylindrical shell panels having cutout is analyzed using the finite element approach. Shell panel and stiffeners are modeled using first-order shear deformation theory and considering displacement compatibility at the stiffener-panel interface.… read more here.
Keywords: shell panels; composite stiffened; stiffened cylindrical; panels cutout ... See more keywords