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Geminus Boeing Project Contract No.EVE-16-2929 <br /> Technology Development CEI Project No. 160731 <br /> 350 <br /> 300 - --TAB t CFD <br /> 250 <br /> 9 <br /> E 200 <br /> a <br /> 150 <br /> w <br /> 100 <br /> `.._1F <br /> 50 <br /> 100 <br /> _150 <br /> c 0 t- 'O W M O 0% 00 N 'O V. N <br /> Location <br /> Figure 29: Comparison of the measured and computed vertical velocity component <br /> around the periphery of the port and starboard horizontal stabilizers (see <br /> Figure 20) for Case 1/Scenarios 1. Note there is a potential mis-numbering <br /> of the measurement locations relative to the CFD measurement locations. <br /> 3.3 Pre-Modification % of LEL Predictions & Comparison <br /> A modified CFD flow volume was developed for computing the % of LEL distribution in the <br /> 45-04 hangar during painting operations and qualitative comparison to % of LEL measurements <br /> taken in the 45-04 hangar. This paint hangar geometry configuration is different than in the <br /> previous sections as it now contains the paint platform "stackers" in typical locations (as <br /> determined by Boeing) and the paint gun representations emitting the gaseous overspray <br /> components. This is known as Case 1/Scenario 2 and the configuration is shown in Figure 30. <br /> 40 <br />