Static Extended Trailing Edge for Lift Enhancement ... - CFD4Aircraft

DOWNLOAD ePAPER

cfd4aircraft.com

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

START NOW

Rigid SETE Under Aerodynamic Loading ?Clamped Elastic Thin Plate Model−1w( x ) = G∫dx∫1 1dx∫2dx∫30xx10x30x30ΔCp( x4)dx4+Ax3/ 6+Bx2/2

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

Rigid SETE Under Aerodynamic Loading ?Clamped Elastic Thin Plate Model−1w( x ) = G∫dx∫1 1dx∫2dx∫30xx10x30x30ΔCp( x4)dx4+Ax3/ 6+Bx2/2