>I don't remember any discussions about
>using the 18% in any configuration other than as a root airfoil tapering
>to a 15% at the tip.

Steve:

Please correct me if I'm wrong but it is my understanding that the center 
section stub wings are a constant cord of 18% thickness and the outer wing 
panels are what taper from 18% at the root to 15% at the tip.

Allen G. Wiesner  KR-2SS/TD S/N 1118
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