Zeige Quelltext Ältere Versionen Links hierher Zu Buch hinzufügen PDF exportieren Seite umbenennen Inhaltsverzeichnis Module „CLT-Plate loaded in plane“ Input data Cross section Fire Internal forces and design factors Results and Output Cross section values Summary of the results Diese Version wurde durch eine neuere bestätigte Version ersetzt.Diese Version (2017/11/15 15:58) ist ein Entwurf. Überprüfungen: 0/1 Dies ist eine alte Version des Dokuments! This page is not fully translated, yet. Please help completing the translation. (remove this paragraph once the translation is finished) Module „CLT-Plate loaded in plane“ Input data The input is divided into: definitions of the cross section specification of parameters concerning structural fire design internal forces (design values) definitions of design factors Cross section See Module CLT-Plate 1D - Continuous beam In diesem Modul kann die Querschnittsbreite nicht verändert werden. Fire See Module CLT-Plate 1D - Continuous beam Fire left / right instead of fire above and below. Internal forces and design factors In the tab „internal forces, stresses and utilization ratio“ it is possible to define the shear force in plane per unit length nxy,d, as well as the design factors. The design method is based on a board width of 150 mm. Results and Output Cross section values The effective stiffnesses of a plate loaded in plane are given in the tab "cross section values" for the full cross section and in case of structural fire design for the charred cross section. The small differences between the extensional stiffnesses Dx and Dy and the effective extensional stiffness EAef in the module CLT-Plate 1D result from the negligence of the extensional stiffness of the cross layers in this module. Summary of the results The calculated substituted thicknesses, stresses as well as utilization ratios of the two mechanisms (Mechanism I – shear and Mechanism II – torsion) are given in the tab "internal forces, stresses and utilization ratios". Furthermore, the utilization ratios, that were calculated based on ETA-08/242 [1] and ETA-09/0036 [2] are given.