. "RIV/46747885:24210/04:24210235" . "The FEM simulation of the deformation of cylindrical air-sprng shell."@en . "[6DBF8FC0EA49]" . "Praha, \u010Cesk\u00E1 republika" . "Praha, \u010Cesk\u00E1 republika" . "Je prezentov\u00E1n postup sestaven\u00ED kone\u010Dn\u011Bprvkov\u00E9ho modelu kompozitn\u00EDho materi\u00E1lu s pry\u017Eovou matric\u00ED vyztu\u017Eenou dv\u011Bma skupinami nit\u00ED. Parametry vyskytuj\u00EDc\u00ED se v navr\u017Een\u00E9m kone\u010Dn\u011Bprvkov\u00E9m modelu jsou ur\u010Deny pomoc\u00ED jednoos\u00FDch a dvouos\u00FDch materi\u00E1lov\u00FDch test\u016F poveden\u00FDch na vzorku dan\u00E9ho kompozitn\u00EDho materi\u00E1lu. Kone\u010Dn\u011Bprvkov\u00FD model a jeho parametry jsou ov\u011B\u0159eny simulac\u00ED vybran\u00FDch materi\u00E1lov\u00FDch test\u016F. Model je aplikov\u00E1n ve v\u00FDpo\u010Dtu deformace pl\u00E1\u0161t\u011B v\u00E1lcov\u00E9 pneumatick\u00E9 pru\u017Einy. V\u00FDsledky kone\u010Dn\u011Bprvkov\u00E9ho v\u00FDpo\u010Dtu jsu porovn\u00E1ny s experiment\u00E1ln\u011B z\u00EDskan\u00FDmi hodnotami."@cs . . . . . "V\u00FDpo\u010Dty konstrukc\u00ED metodou kone\u010Dn\u00FDch prvk\u016F 2004, listopad 2004" . "RIV/46747885:24210/04:24210235!RIV/2005/MSM/242105/N" . . . . "\u00DAstav termomechaniky AV \u010CR" . "593632" . "The FEM simulation of the deformation of cylindrical air-sprng shell."@en . "V\u00FDpo\u010Det deformace pl\u00E1\u0161t\u011B v\u00E1lcov\u00E9 pneumatick\u00E9 pru\u017Einy" . "Z(MSM 242100001)" . . "Urban, Robert" . . "%2280;90%22" . "2004-01-01+01:00"^^ . "Marvalov\u00E1, Bohdana" . . . "24210" . . . "Komposite material, FEM, Rubber, Experiment"@en . "80-214-2489-4" . . "V\u00FDpo\u010Det deformace pl\u00E1\u0161t\u011B v\u00E1lcov\u00E9 pneumatick\u00E9 pru\u017Einy" . . "V\u00FDpo\u010Det deformace pl\u00E1\u0161t\u011B v\u00E1lcov\u00E9 pneumatick\u00E9 pru\u017Einy"@cs . "10"^^ . "2"^^ . "Je prezentov\u00E1n postup sestaven\u00ED kone\u010Dn\u011Bprvkov\u00E9ho modelu kompozitn\u00EDho materi\u00E1lu s pry\u017Eovou matric\u00ED vyztu\u017Eenou dv\u011Bma skupinami nit\u00ED. Parametry vyskytuj\u00EDc\u00ED se v navr\u017Een\u00E9m kone\u010Dn\u011Bprvkov\u00E9m modelu jsou ur\u010Deny pomoc\u00ED jednoos\u00FDch a dvouos\u00FDch materi\u00E1lov\u00FDch test\u016F poveden\u00FDch na vzorku dan\u00E9ho kompozitn\u00EDho materi\u00E1lu. Kone\u010Dn\u011Bprvkov\u00FD model a jeho parametry jsou ov\u011B\u0159eny simulac\u00ED vybran\u00FDch materi\u00E1lov\u00FDch test\u016F. Model je aplikov\u00E1n ve v\u00FDpo\u010Dtu deformace pl\u00E1\u0161t\u011B v\u00E1lcov\u00E9 pneumatick\u00E9 pru\u017Einy. V\u00FDsledky kone\u010Dn\u011Bprvkov\u00E9ho v\u00FDpo\u010Dtu jsu porovn\u00E1ny s experiment\u00E1ln\u011B z\u00EDskan\u00FDmi hodnotami." . "V\u00FDpo\u010Det deformace pl\u00E1\u0161t\u011B v\u00E1lcov\u00E9 pneumatick\u00E9 pru\u017Einy"@cs . "1"^^ . . "The paper deals with a simulation of hyperelastic rubber materials reinforced by threads of multifilament. The threads are aligned in one or more layers. Materials like those have substantial directional properties and can be classed with a group of anistropic hyperelastic materials. Further, a finite element model whose mechanical properties were determined from experimental tests for the given material was made up. The material model verification was realized by confrontation of experimental data andesults obtained by using finite element method. The model material was applied in a computation of air spring sleeve deformation by finite element method using the software ANSYS. Results of the computation are compared with experimental values measuredn testing parts."@en .