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A 6 series or laminar flow airfoil's 'drag bucket' on a polar plot of Cl vs Cd shows; The range of angles of attack that
A 6 series or laminar flow airfoil's 'drag bucket' on a polar plot of Cl vs Cd shows; The range of angles of attack that produce less lift )The range of angles of attack that can save fuel O The range of angles of attack that produce less drag O Both b and c above
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