Characterization of Oscillatory Lift in MFC Airfoils

dc.contributor.authorLang Jr, Joseph Reagleen
dc.contributor.committeechairKochersberger, Kevin B.en
dc.contributor.committeememberDevenport, William J.en
dc.contributor.committeememberTarazaga, Pablo Albertoen
dc.contributor.departmentMechanical Engineeringen
dc.date.accessioned2014-11-26T09:00:23Zen
dc.date.available2014-11-26T09:00:23Zen
dc.date.issued2014-11-25en
dc.description.abstractThe purpose of this research is to characterize the response of an airfoil with an oscillatory morphing, Macro-fiber composite (MFC) trailing edge. Correlation of the airfoil lift with the oscillatory input is presented. Modal analysis of the test airfoil and apparatus is used to determine the frequency response function. The effects of static MFC inputs on the FRF are presented and compared to the unactuated airfoil. The transfer function is then used to determine the lift component due to cambering and extract the inertial components from oscillating airfoil. Finally, empirical wind tunnel data is modeled and used to simulate the deflection of airfoil surfaces during dynamic testing conditions. This research serves to combine modal analysis, empirical modeling, and aerodynamic testing of MFC driven, oscillating lift to formulate a model of a dynamic, loaded morphing airfoil.en
dc.description.degreeMaster of Scienceen
dc.format.mediumETDen
dc.identifier.othervt_gsexam:3689en
dc.identifier.urihttp://hdl.handle.net/10919/50935en
dc.publisherVirginia Techen
dc.rightsIn Copyrighten
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/en
dc.subjectMorphing Airfoilen
dc.subjectPiezoelectricityen
dc.subjectMacro-Fiber Compositeen
dc.subjectOscillatory Liften
dc.subjectSmart Wingen
dc.titleCharacterization of Oscillatory Lift in MFC Airfoilsen
dc.typeThesisen
thesis.degree.disciplineMechanical Engineeringen
thesis.degree.grantorVirginia Polytechnic Institute and State Universityen
thesis.degree.levelmastersen
thesis.degree.nameMaster of Scienceen

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