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sligo565
Mar 21, 2008, 11:42 AM
Hi Guys,

Could anyone tell me how to calculate the Drag Polar?

Is it:

1/(pi x A x e)

Where A = Aspect Ratio
e = Oswald Efficiency Factor

I have graphs of CL vs CD and i was just wondering do i use this or do i use the CDmin as an estimation?

eflightray
Mar 22, 2008, 09:38 AM
Sorry I haven't a clue, I never fly where there are parasites or polar bears :D

But I did find this with a quick search, no idea if it's what you want but it looks and uses those sort of words. ;) Me? I just chuck them in the air and hope. :D

The Dreese Airfoil Primer (http://www.dreesecode.com/primer/airfoil3.html)

Hope it's of some use.

vintage1
Mar 22, 2008, 10:10 AM
Drag Polar?

That's "Eskimo Nell" isn't it?

;)