Control authority of V-tail vs. Cruciform - Page 7 - RC Groups
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Nov 22, 2012, 07:59 AM
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hi kevin, i came across this airfoil which seems pretty impressive.

i was thinking of altering it to a 1% camber with max camber at about .5c

i'm looking for a Cm curve from about -.02 at < 5 deg AoA and ramps up to a max of about +.02.

what do you think?
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