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alGemnus Boeing Project Contract No.EVE-16-2929
<br /> Technologyi Development CEI Project No. 160731
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<br /> Figure 54: Top: Paint gun locations and painting direction indicators for Case 2/Scenario
<br /> lb simulation. Bottom: Plot of velocities magnitudes at all active primary and
<br /> secondary ceiling air supply locations.
<br /> Figure 55 through Figure 57 depicts the size of the computed >2% of LEL volatile volumes
<br /> around the aircraft with the C 1 D 1/C 1 D2 boundaries and building outline superimposed. These
<br /> are similar in size and extent to that computed for Case 1/Scenario 2 and all are well within the
<br /> C1D1/C1D2 boundaries. Figure 58 shows the computed % of LEL values at the exhaust
<br /> locations and are all well below the 2% of LEL level as expected. The computed % of LEL
<br /> 59
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