Laserfiche WebLink
. . <br /> ILGeminus Boeing Project Contract No.EVE-16-2929 <br /> Technology Development CEI Project No. 160731 <br /> N. <br /> I, lliAllam. <br /> IV <br /> .. .• ir010 <br /> lb <br /> t 00 ( In <br /> 01 • 0 ,. <br /> 111 <br /> ,, • ,,;,.4: 0.00,000 . . 10...„,, <br /> -..,--:-=,-,,::-..71: -:7:.7.--f---,..-",,-,-. , .4.11r I 1 <br /> .4 ?*r. --:1,--,...-4- <br /> / . '- <br /> t `' �-....! � <br /> ;,..*- <br /> il r � ni/ i�;-:_� . itik�-- <br /> ':. . _!i liktio..;' <br /> ce <br /> i/pqpiT.-,„,- -• - ,--,_-, __ --,.. <br /> ..416 ' .4. ' 41I% <br /> ;low- -, A <br /> `1 <br /> Velocity(ft/s) <br /> 0.0 4.0 8.0 12.0 16.0 �0 <br /> Figure 16: Plot of velocity magnitudes at all active supply and exhaust locations for <br /> Case 1/Scenario 1 <br /> , I,t, 4 f Al I i 1 i i .1 1 ' I 14 kaki <br /> Y Mean Velocity:Magnitude(ft/s) <br /> Z X 0. 2. 4. 6. 8. 10. 12. 14. 16.`Y 18. 20. <br /> Figure 17: Computed airflow velocity magnitude contours on the aircraft/hangar <br /> symmetry plane for Paint Mode (Case 1/Scenario 1). <br /> 28 <br />