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Thin Airfoil Theory - Virginia Tech
Example 1 – Symmetric Foil An airfoil has a straight camber line defined as: Determine the aerodynamic characteristics and vortex sheet strength. 0 ( )cos() 2 n d dx d B c n V x 0 c 0 x/c 21 (1 cos ) u t c l ( ) 4 ( 1 2) C 1 C 1 B B c l x mx C l 2 (B 0 B 1) c /c 0
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