Bruce wrote:

>> No i didn't include that. Do they measure the area directly between the leading and trailing edges of wings? Cant see it contributing much to lift at low angles of attack but hey..if that's the accepted convention! In this case it would at about 16 sq ft...<<

Yep, leading to trailing edges, everything that's between the two wings. I checked last night and found where the airfoil on that plane is likely the 23012, which has a stall curve that has a rather sharp break to it. Having said that, it's been used on a lot of old factory planes, but probably with more washout than that wing has.

Mark Langford
m...@n56ml.com
http://www.n56ml.com


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