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S031 <br />v <br />/i V t T t AJ R, •r Q L A ,v o f/ L L F. K i° . LPROJECTN F')(I- hi�?F NO. <br />COMP.M T _CHK. REV. ___2._ Z PAGES <br />DATE y / // 14 S_ DATE -DATE <br />- <br />It L (f vc./r7)0N �,= f/fC f02 v,= S/r IF— <br />/ <br />l� r <br />/I rt /, /t L L 0 V--/ it /Y I- f STn it Jv _ X <br />! FfI:F'GT/vl Sr�/tr,.. ee <br />f : S. -r- / 4.c I, 2. ') I <br />� != S ) <br />(1) Extrusion Lap [6 mm] (*) <br />y) (2) Extrusion Fillet [6-7 mm] (*) <br />;2) 3 ion Lap�(135mml (*)(3) (4)Fusion [4 mm <br />(4) <br />0.0 M 1.0 1.5 20 25 3.0 <br />Average Tensile Strain, ea (9'a) <br />Geomembrane Thickness: <br />2 mm (80 mils) <br />Seam Width: <br />38 mm (1.5 in.) <br />Figure 9. Tensile strain due to geomembrane bending next to a seam, Eb, as a function of the <br />average tensile strain, E_, in the geomembrane. The charts are applicable to seams <br />that are free to rotate; in the case of seams that are subjected to normal stresses that <br />limit their ability to rotate, the bending strains should be less than indicated on the <br />charts. (*) Note: The value indicated in square brackets is the total seam thickness, <br />i.e., thickness of extrudate, if any, plus thickness of two geomembrane layers. <br />