Experimental and finite element numerical studies on the post-buckling behavior of composite stiffened panels
Sign Up to like & getrecommendations! Published in 2019 at "Mechanics of Advanced Materials and Structures"
DOI: 10.1080/15376494.2019.1701151
Abstract: Abstract Aircraft composites structures are typically made using stiffened skin construction as it provides a minimum weight solution to many design problems. However, designers are reluctant to allow composite stiffened structures to operate in the… read more here.
Keywords: finite element; post buckling; stiffened panels; experimental finite ... See more keywords
Buckling behavior of laminated composite stiffened cylindrical shell panels having cutout for different parametric variations
Sign Up to like & getrecommendations! Published in 2022 at "Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science"
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