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dc.contributor.advisorPlatzer, Max F.
dc.contributor.advisorHebbar, S.K.
dc.contributor.authorRiester, Peter J.
dc.date.accessioned2013-01-23T21:59:18Z
dc.date.available2013-01-23T21:59:18Z
dc.date.issued1993-06
dc.identifier.urihttps://hdl.handle.net/10945/26422
dc.description.abstractIn this thesis several incompressible oscillatory flow and flutter problems were investigated. First, a previously developed unsteady panel code was modified so that systematic comparisons with Theodorsen's classical theory could be accomplished. It was found that the panel code is in excellent agreement with the Theodorsen results. Second, the panel code was applied to the analysis of bending- torsion flutter. Again, general agreement with Theodorsen's flutter predictions was obtained. In the experimental part of the thesis two flow visualization experiments were performed. First, the vortical flow patterns generated by an airfoil executing harmonic plunge oscillations were visualized. In the second experiment, the interference effects between a stationary airfoil and a small vane executing plunge oscillations were explored.en_US
dc.description.urihttp://archive.org/details/acomputationalnd1094526422
dc.format.extent149 p.en_US
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.titleA computational and experimental investigation of incompressible oscillatory airfoil flow and flutter problems.en_US
dc.typeThesisen_US
dc.contributor.corporateNaval Postgraduate School
dc.contributor.schoolNaval Postgraduate School
dc.contributor.departmentAeronautical Engineering
dc.subject.authorFlutteren_US
dc.subject.authorTheodorsen comparison with panel code U2DDFen_US
dc.subject.authorEnhanced liften_US
dc.subject.authorFlow visualizationen_US
dc.description.serviceLieutenant Commander, United States Navyen_US
etd.thesisdegree.nameM.S. in Aeronautical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.disciplineAeronautical Engineeringen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US
dc.description.distributionstatementApproved for public release; distribution is unlimited.


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