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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Comparison between SETE and Gurney FlapBenefit Margin <strong>for</strong> PassiveFlow Control in CruiseFlightEXP6 ΔC−7 CDD+97ΔCCLL=g>0

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Comparison between SETE and Gurney FlapBenefit Margin <strong>for</strong> PassiveFlow Control in CruiseFlightEXP6 ΔC−7 CDD+97ΔCCLL=g>0

Comparison between SETE and Conventional FlapCFD

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 and 10: Lift Enhancement by SETEEXP
Page 11 and 12: Lift Enhancement by SETECFDCamber E
Page 13: MATLAB Handle GraphicsComparison be
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