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This diagram demonstrates optimal sizing for the wing surface area and aspect ratio. The<br />
final wing geometry was selected based upon this plot in conjunction with a number of<br />
constraints, such as those in the previous charts.<br />
Cost/ton-nm ($)<br />
0.600<br />
0.590<br />
0.580<br />
0.570<br />
0.560<br />
0.550<br />
0.540<br />
0.530<br />
0.520<br />
800<br />
900<br />
1000<br />
<strong>DOC</strong> <strong>vs</strong> AR & Wing Area<br />
1100<br />
1200<br />
1300<br />
8<br />
10<br />
12<br />
14<br />
16<br />
18<br />
This snapshot of Jetsizer’s<br />
Mission input page (left) shows<br />
the results of the code and<br />
includes checks for mission<br />
constraints<br />
The image shown shows the<br />
results of an aircraft planform<br />
that was run with intentionally<br />
poor configuration in order to<br />
demonstrate the constraint<br />
checks.<br />
Note: The Ascian Ray PASSED<br />
these checks.<br />
P a g e | 10
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