Static Extended Trailing Edge for Lift Enhancement ... - CFD4Aircraft
Static Extended Trailing Edge for Lift Enhancement ... - CFD4Aircraft
Static Extended Trailing Edge for Lift Enhancement ... - CFD4Aircraft
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Thin-Airfoil Theoretical Interpretation <strong>for</strong> SETE−1⎡ 2(1 + τ ) ⎤Δ CL= 2⎢1 +c+AR ⎥⎣ ⎦[ πε α + ( 1 + ε )tanδ( π −θsinθ)]c