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Old 04-30-2012, 05:41 PM   #2 (permalink)
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When you consider a 12.5% thickness fuselage with the aft-body completely cut away,at Cd 0.374,then the same fuselage with the tail restored,at Cd 0.066,you realize the significance of the trailing surface of any vehicle.
So there's no element of surprise with your results.I hope you have a blast passing gas stations with the new combination.
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