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

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

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

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MATLAB Handle GraphicsMATLAB Handle GraphicsL/D of NACA0012 with SETEEXP• L/D vs. CL curves are collapsed <strong>for</strong> different deflection angles• Zero-lift drag and Oswald efficiency remain unchanged<strong>Lift</strong> <strong>Enhancement</strong> at the Minimum DragPenalty <strong>for</strong> Cruise Flight

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MATLAB Handle GraphicsMATLAB Handle GraphicsL/D of NACA0012 with SETEEXP• L/D vs. CL curves are collapsed <strong>for</strong> different deflection angles• Zero-lift drag and Oswald efficiency remain unchanged<strong>Lift</strong> <strong>Enhancement</strong> at the Minimum DragPenalty <strong>for</strong> Cruise Flight

<strong>Lift</strong> <strong>Enhancement</strong> by SETECFDCamber Effect!Camber Effect!

Page 3 and 4: Objectives• Understand the aerody
Page 5 and 6: Technical Approaches —Combination
Page 7 and 8: Computational Fluid Dynamics Calcul
Page 9: Lift Enhancement by SETEEXP
Page 13 and 14: MATLAB Handle GraphicsComparison be
Page 15 and 16: Comparison between SETE and Convent
Page 17 and 18: Comparison of SETE, Gurney, and Con
Page 19 and 20: Rigid SETE Under Aerodynamic Loadin
Page 21 and 22: Responsive Skins forFlexible Extend
Page 23: Concluding Remarks• Integrating C