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Investigation of Transonic Drag Computations in Aerodynamic ...

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<strong>Investigation</strong> <strong>of</strong> <strong>Transonic</strong> <strong>Drag</strong> <strong>Computations</strong> <strong>in</strong> APAS<br />

Trial 1 WAVDRAG<br />

Area (ft 2 )<br />

90<br />

80<br />

70<br />

60<br />

50<br />

40<br />

30<br />

20<br />

10<br />

0<br />

0 20 40 60 80 100<br />

x location (ft)<br />

Figure 34. WAVDRAG Area Build-up for Trial 1<br />

The shape <strong>of</strong> the area build-up for the trial 1 configuration <strong>in</strong> WAVDRAG is<br />

shown <strong>in</strong> Figure 34. WAVDRAG outputs the area build-up as the average <strong>of</strong> that <strong>of</strong> the<br />

areas obta<strong>in</strong>ed from the cutt<strong>in</strong>g planes at each roll angle θ. The curve is <strong>of</strong> the same<br />

shape as the APAS build-up, which demonstrates that the two programs are analyz<strong>in</strong>g the<br />

same configuration and are generat<strong>in</strong>g similar, if not identical, sets <strong>of</strong> equivalent bodies.<br />

The maximum area reached <strong>in</strong> the WAVDRAG figure is that <strong>of</strong> a circle with a radius <strong>of</strong> 5<br />

ft, which is the maximum cross-sectional area <strong>of</strong> trial 1.<br />

Jeff Miller 30

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