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dc.contributor.authorMorman, Joshua
dc.description.abstractBiological flapping wing flyers achieve flight maneuverability and efficiency in low speed flight environments that has not been replicated by man-made flyers. Micro Air Vehicle (MAV) design goals are to develop flyers that maintain flight in environments that biological flyers excel in which includes low speeds, hovering, and urban settings. This flight is characterized by flow phenomena that are not well understood such as: flow separation and vortical flow. The goal of this study is to perform a literature review about the aerodynamics of flapping flight and discuss the application to MAV design. The study will evaluate the design initiatives of MAV. Experimental and computational test methods are reviewed. Low Reynolds number aerodynamics are studied. The effects of airfoil aeroelasticity and geometry are discussed. Then, the application of the aerodynamics to flapping motions are reviewed. Finally, operational MAV designs are studied and recommendations are made to further advance the state of the art.en_US
dc.publisherNorth Dakota State Universityen_US
dc.rightsNDSU Policy 190.6.2
dc.titleLiterature Review of the Aerodynamics of Flapping Flight in Micro Air Vehicle Applicationsen_US
dc.typeMaster's paperen_US
dc.date.accessioned2014-11-28T22:34:56Z
dc.date.available2014-11-28T22:34:56Z
dc.date.issued2014
dc.identifier.urihttp://hdl.handle.net/10365/24471
dc.subject.lcshMicro air vehicles.en_US
dc.subject.lcshMicro air vehicles -- Wings.en_US
dc.subject.lcshAerodynamics.en_US
dc.subject.lcshReynolds number.en_US
dc.rights.urihttps://www.ndsu.edu/fileadmin/policy/190.pdf
ndsu.degreeMaster of Science (MS)en_US
ndsu.collegeEngineeringen_US
ndsu.departmentMechanical Engineeringen_US
ndsu.programMechanical Engineeringen_US
ndsu.advisorSuzen, Yildirim B.


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