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

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Flexible MEMS Array(Pressure, Humidity, Temperature, Microphone, 2-axis Accelerometer)Absolute PressurePressure,Humidity, Temp.MEMS microphonesSOI (Silicon on Insulator)High Temp. Press. & Temp SensorsUp to 240 CTwo-axis accelerometerMEMS sensors on flexible skin have been designedand will be characterized.NASA Langley
Concluding Remarks• Integrating CFD and experiments capabilities in theresearch process provide countless benefits:- Scholarship-Cost- Time to Market- Team Leadership-Education‣Long Term Vision, Planning, and Funding
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 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: Responsive Skins forFlexible Extend

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

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