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SD 11 <br /> /A V L7 tA,/ P. TQ L1+ Nf)P/L L 1' x /® , PROJECT <br /> /t L L ,✓ L-3 L -Ar-'T /1 /Iv Iy n- t-i 17F FILE NO. <br /> COMP. nn / T CHK. REV. PAGE2�OF Z. PAGES <br /> DATE -? P1 14S- DATE DATE <br /> C /r L C V L. /t7 1 J n/ 0 -ItGTO/Z o i= $.'r F r *r C F ) <br /> ,y1 it A /t LLD57eelt.W <br /> l e Ff�F. CT/v! StR�t!w <br /> e <br /> fS - S. rl etc 1 , 2 I <br /> (1) E=usion Lap [6 mm] M <br /> 3-5 h y (2) Extrusion Fillet [6-7 mm] (*) <br /> i tg-2MMI ( (2) on [5 mm] (*) <br /> � 3.0 I I ( (3) �, (4�FusiOn [4 i <br /> 2.5 (4) <br /> Geomembrane Thickness. <br /> 1 S 2 mm (80 ) <br /> - m <br /> Seam Width: <br /> os 38 m (1.5 in.) <br /> 0.0 T 71 <br /> 0.0 0.5 1.0 1.5 2.0 2.5 3.0 <br /> Average Tensile strain.Ea <br /> Figure 9. Tensile strain due to geomembrane bending next to a seam, 4, as a function of the <br /> average tensile strain, E_, in the geomembrane. The charts are applicable to seams <br /> that are ftee 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 />