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

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Teaming —Combination of Experimental, Computational and Theoretical MethodsOrganization:Western Michigan Univ. - CFD & EXPNASA Langley Research Center - EXPPersonnel:Faculty (2), Research Scientist (1), Post-Doc (1), GS-Doc (1),GS-MS(1), UG students(2).EXPFaculty OnePost DocGS-MSUG StudentsResearch ScientistFaculty TwoGS-DocCFDCommunications:Meetings, Emails, Calls, Site Visits, Hall-Way Conversations.Immersive Integration.
Computational Fluid Dynamics CalculationsSolver:Commercial Code: RANS using FLUENT, CFXIn-House Code: 3D RANS solver with immerseboundary method, Incompressible, Second-Order,Turbulence Modeling.Meshing:Structured and unstructured using ICEM and in-houseGrid Independence. Grid Convergence.Validation:NACA0012 Laminar and Turbulent.
Page 3 and 4: Objectives• Understand the aerody
Page 5: Technical Approaches —Combination
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 and 22: Responsive Skins forFlexible Extend
Page 23: Concluding Remarks• Integrating C

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

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