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en:clt:hotspot:software:cltdesigner:manual:modul_plate_in_plane [2017/11/15 16:53] – [Querschnittswerte] Alexandra Thielen:clt:hotspot:software:cltdesigner:manual:modul_plate_in_plane [2020/10/28 10:13] (aktuell) Alexandra Thiel
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-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}} {{ en:clt:hotspot:software:cltdesigner:manual:modul_plate_in_plane:gesamtscheibe.png?600 |CLT-Plate loaded in plane}}
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 ==== Cross section ==== ==== 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 ==== ==== 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 ==== ==== 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 mmFIXME+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}} {{ en:clt:hotspot:software:cltdesigner:manual:modul_plate_in_plane:schnittkrafteingabe_scheibe.png |Input - internal forces and design factors}}
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 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 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.
  
-{{ en:clt:hotspot:software:cltdesigner:manual:modul_plate_in_plane:querschnittswerte_scheibe.png?600 |Cross section values}}+{{ 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. 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> </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 „SchnittgrößenSpannungen und Ausnutzung“ werden die berechneten ErsatzdickenSpannungen sowie die Ausnutzungsgrade der beiden Mechanismen (Mechanismus – Schub und Mechanismus – Torsionangezeigt.+Furthermorethe utilization ratiosthat 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~~
  • en/clt/hotspot/software/cltdesigner/manual/modul_plate_in_plane.1510761224.txt.gz
  • Zuletzt geändert: 2017/11/15 16:53
  • von Alexandra Thiel