Thread: Drag per aft-body length/roof angle
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Old 10-17-2015, 05:25 PM   #53 (permalink)
aerohead
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2.2:1 streamline body = Cd 0.04
Here's Hucho's drag table from his 2nd-Edition,1987.
I've highlighted the teardrop I used for the aft-body of the 'Template.'
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