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sa 500 starlet airfoil
I'm looking for the right airfoil data for the starlet homebuilt
I would like to start first of all making a mockup of the wing to understand difficults and may be later with the right materials I have the drawings of the plane but I cannot understand why there is difference between the CYH(is it?) standard airfoil(Max Thck=11,7%) and the plans.May be because of the hardcopy scale,infact the MAX thickness on the drawings result to be 12,7%(circa).Unfortunately plans are not completely dimensioned,so I should make parts copying them and I don'like it What can I do? Somebody can help me? Thanks |
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