Quote:
Originally Posted by drmiller100
hmmmm..
Thank you for running those numbers. Not at all what I was hoping for in terms of results.
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I did a rough look at your project scaling 45" at max camber point.
*at 24" aft you'd be at approx. 43.82"
*at 48" aft,40.48"
*at 72" aft,35.0"
At this terminus for the body,it would put you at 42.5% of the 'Template' aft-body with a potential for around Cd 0.17 if everything is very clean up to that point.(think AEROCIVIC)