1998
DOI: 10.1016/s0263-8223(98)00006-3
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Local behavior of discretely stiffened composite plates and cylindrical shells

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Cited by 29 publications
(11 citation statements)
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“…10/3 (L: edge length of the RVE, D: diameter of the particles) allows an appropriate prediction of effective material properties [138]. For laminated composites, layer-wise shell theory can be applied [142].…”
Section: Simulation Approachesmentioning
confidence: 99%
“…10/3 (L: edge length of the RVE, D: diameter of the particles) allows an appropriate prediction of effective material properties [138]. For laminated composites, layer-wise shell theory can be applied [142].…”
Section: Simulation Approachesmentioning
confidence: 99%
“…1, are used in practical applications. Many researchers have devoted themselves to studying grid-stiffened composite panels [5,6,7,8,9]. The discrete stiffener and the smeared stiffener methods are two main methods used to study behaviour of such structures.…”
Section: Introductionmentioning
confidence: 99%
“…A survey of more recent relevant literature leads to the conclusion that on the one hand, the problem of the buckling and postbuckling of stiffened isotropic and orthotropic laminated composite plates and shells is well understood and has been challenged using a broad variety of computational approaches, mostly using the finite element method [19][20][21][22][23][24][25][26][27][28][29], the finite strip method [30][31][32][33], or other numerical approaches like the Ritzmethod [25,[34][35][36][37][38]. However, even though such sophisticated approaches usually work with superior accuracy and are generally applicable to virtually any structural situation, especially purely numerical methods are not an option when a stiffened plate structure is to be assessed e.g.…”
Section: Introductionmentioning
confidence: 99%