Differences

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--- en:clt:hotspot:software:cltdesigner:manual:modul_plate_in_plane [2017/11/15 16:53] – [Cross section values] Alexandra Thiel
+++ en:clt:hotspot:software:cltdesigner:manual:modul_plate_in_plane [2020/10/28 10:13] (current) – Alexandra Thiel
@@ Line 1: / Line 1: @@
-FIXME **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" ======
-====== Module „CLT-Plate loaded in plane“ ======
 {{ en:clt:hotspot:software:cltdesigner:manual:modul_plate_in_plane:gesamtscheibe.png?600 |CLT-Plate loaded in plane}}
@@ Line 14: / Line 12: @@
 ==== Cross section ====
-See [[modul_plate1d_continuousbeam#cross_section|Module CLT-Plate 1D - Continuous beam]]
+The input is the same as for the [[en:clt:hotspot:software:cltdesigner:manual:modul_plate1d_continuousbeam|Module "CLT-Plate 1D - Continuous beam"]].
-In diesem Modul kann die Querschnittsbreite nicht verändert werden.
+++++ Show description |
+{{section> en:clt:hotspot:software:cltdesigner:manual:modul_plate1d_continuousbeam#cross_section&inline&permalink&noheader}}
+++++
+In this module it is not possible to change the cross sectional width.
 ==== Fire ====
-See [[modul_plate1d_continuousbeam#brand|Module CLT-Plate 1D - Continuous beam]]
+The input is the same as for the [[en:clt:hotspot:software:cltdesigner:manual:modul_plate1d_continuousbeam|Module "CLT-Plate 1D - Continuous beam"]].
-Brand links / rechts statt Brand oben / unten.
+++++ Show description |
+{{section> en:clt:hotspot:software:cltdesigner:manual:modul_plate1d_continuousbeam#fire&inline&permalink&noheader}}
+++++
+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 n<sub>xy,d</sub>, as well as the design factors. The design method is based on a board width of 150 mm. FIXME
+In the tab „internal forces, stresses and utilization ratio“ it is possible to define the shear force in plane per unit length n<sub>xy,d</sub>, as well as the design factors. The design method is based on a board width which is chosen when defining the cross section.
 {{ en:clt:hotspot:software:cltdesigner:manual:modul_plate_in_plane:schnittkrafteingabe_scheibe.png |Input - internal forces and design factors}}
@@ Line 35: / Line 41: @@
 {{ en:clt:hotspot:software:cltdesigner:manual:modul_plate_in_plane:querschnittswerte_scheibe.png |Cross section values}}
-<WRAP center round info 100%>
+<WRAP center info 100%>
 The small differences between the extensional stiffnesses D<sub>x</sub> and D<sub>y</sub> and the effective extensional stiffness EA<sub>ef</sub> in the module CLT-Plate 1D result from the negligence of the extensional stiffness of the cross layers in this module.
 </WRAP>
-==== Zusammenfassung der Ergebnisse ====
+==== 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".
-In der Karteikarte „Schnittgrößen, Spannungen und Ausnutzung“ werden die berechneten Ersatzdicken, Spannungen sowie die Ausnutzungsgrade der beiden Mechanismen (Mechanismus – Schub und Mechanismus – Torsion) angezeigt.
+Furthermore, the utilization ratios, that were calculated based on ETA-08/242 [(:ref:eta_08_0242_2009)] and ETA-09/0036 [(:ref:eta_09_0036_2009)] are given.
-Zum Vergleich werden auch die Ausnutzungsgrade angelehnt an ETA-08/242 [(:ref:eta_08_0242_2009)] und ETA-09/0036 [(:ref:eta_09_0036_2009)] berechnet und angezeigt.
+{{ en:clt:hotspot:software:cltdesigner:manual:modul_plate_in_plane:zusammenfassung_scheibe.png |Summary of the results}}
-{{ clt:hotspot:software:cltdesigner:manual:modul_plate_in_plane:zusammenfassung_scheibe.png?600 |Zusammenfassung der Ergebnisse}}
+~~DISCUSSION~~