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dc.contributor.authorJones, K.D.
dc.contributor.authorDavids, S.
dc.contributor.authorPlatzer, M.F.
dc.date1999
dc.date.accessioned2013-11-06T21:14:01Z
dc.date.available2013-11-06T21:14:01Z
dc.date.issued1999
dc.identifier.citationJones, K.D., Davids, S. and Platzer, M.F., "Oscillating-Wing Power Generator," ASME/JSME Joint Fluids Engineering Conference, San Francisco, California, July 1999.
dc.identifier.urihttp://hdl.handle.net/10945/37213
dc.descriptionASME/JSME Joint Fluids Engineering Conference, San Francisco, California, July 1999.en_US
dc.description.abstractNumerical and experimental methods are described for the investigation of an oscillating-wing generator or wingmill. The numerical approach applies a previously developed, unsteady, incompressible panel method incorporating a non-linear, deforming wake model to compute the unsteady flow about an airfoil undergoing specified pitch and plunge motions. An experimental model is described which can duplicate much of the parameter-space available to the panel method. Numerical results are presented demonstrating configurations that yield high efficiencies. Results are compared to the wingmill experiments of McKinney and DeLaurier.en_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, may not be copyrighted.en_US
dc.titleOscillating-Wing Power Generatoren_US
dc.typeConference Paperen_US
dc.contributor.departmentDepartment of Mechanical and Aerospace Engineering


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