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. . <br /> ILGeminus Boeing Project Contract No.EVE-16-2929 <br /> Technology Development CEI Project No. 160731 <br /> .......4 <br /> r� <br /> 4 "Aliclinii. --;---17- 1:11.-_-;17 ----2':- - ' / <br /> ��Wig!mitt"1-'O <br /> . •' <br /> Ji <br /> r• } • <br /> F. <br /> i. <br /> i <br /> Figure 69: Location of the high bay stacker during all Case 3 scenarios. High bay <br /> stacker located so that painter can exit onto the HSP configured for painting <br /> bottom of the horizontal stabilizer. HSP located at 6-1/2' below HS bottom <br /> surface for Case 3/Scenario lb. <br /> Figure 70 depicts the locations and orientations of the spray guns used in this simulation and <br /> which air supplies and exhausts are active by plotting velocity vectors on each air supply and <br /> exhaust surface. Figure Figure 71 through 73 depicts the size of the >2% LEL volumes around <br /> g gP <br /> the aircraft with the C 1D 1 and C 1D2 3D boundaries superimposed over the hanger outline for <br /> reference. Figure 74 depicts the % of LEL levels at the entrances of the floor exhausts. Figure <br /> 75 through Figure 83 show contour x-sections of% of LEL for Case 3/Scenario 1 b at various the <br /> various locations denoted in Figure 59. <br /> 70 <br />