20.500.12556/RUL-32199 On composite shell models with a piecewise linear warping function A multilayered shell model accounting for a piecewise linear (i.e. zig-zag) distribution of displacements through the laminate thickness is discussed. The model has seven unknown kinematic variables: three displacements of the middle surface, two rotations of the shell director and two displacements associated with the wrinkling of the laminate cross-sections. The initial transverse shear stress field is introduced, and the constitutive relations are then relaxed in the framework of the variational principle. Finite element solutions obtained with this kind of model are compared with the analytical solutions for the case of cylindrical shell bending. composite shell finite element zig-zag function interlaminar continuity kompozitne lupine končni elementi zig-zag funkcija medlaminarna zveznost true false false Elsevier Angleški jezik Angleški jezik Neznano 2015-07-10 10:13:02 2015-07-10 10:13:02 2022-11-21 15:47:34 0000-00-00 00:00:00 2002 0 0 Str. 163-171 Vol. 59 Vol. 59 2002 0000-00-00 NiDoloceno NiDoloceno NiDoloceno 0000-00-00 0000-00-00 0000-00-00 624.074.4 0263-8223 1794145 15329285 CS_2003_brank_k.pdf CS_2003_brank_k.pdf 1 1FF1C3B96CDECFFC9D4D54A200D6A9BE 562f870ccc387040ac76fe6ba9ab543c4ca8d75ea812861976c9ece8f710377b 14f086b6-a1ae-11eb-a523-00155dcfd717 20.500.12556/rul/f3dccd6f-f0bf-4b12-b1fd-851a75c31ac9 https://repozitorij.uni-lj.si/Dokument.php?lang=slv&id=85710 Fakulteta za gradbeništvo in geodezijo 0 0 0