Fluid-Structure Interaction Modeling of MAV Flapping-Wing Aerodynamics

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dc.contributor.advisorTezduyar, Tayfun E.en_US
dc.contributor.committeeMemberMeade, Andrewen_US
dc.contributor.committeeMemberAkin, Eden_US
dc.contributor.committeeMemberTakizawa, Kenjien_US
dc.creatorMontel, Kenneth Keefen_US
dc.date.accessioned2016-01-28T22:05:05Zen_US
dc.date.available2016-01-28T22:05:05Zen_US
dc.date.created2015-05en_US
dc.date.issued2015-04-23en_US
dc.date.submittedMay 2015en_US
dc.date.updated2016-01-28T22:05:05Zen_US
dc.description.abstractThis thesis is on computational fluid-structure interaction (FSI) modeling of bioinspired flapping-wing aerodynamics of a micro aerial vehicle (MAV). The wing motion is prescribed partially, based on the high-speed, multi-camera video recordings of an actual locust in a wind tunnel. The rest of the wing motion comes from the deformation response of the wing structure in the FSI solution. Varying the wing structure design would vary that deformation response and thus influence the aerodynamic performance. This makes the FSI modeling valuable in wing design. The computations are challenging because the motion of the wings is partially based on data extracted from the video recordings of the actual locust. Furthermore, computing the correct aerodynamical forces acting on the wings requires a method that can, with a good level accuracy, resolve the flow field near the wing surfaces. The core computational technology is the space-time variational multiscale (ST-VMS) method. The ST-VMS method is a moving-mesh technique, which enables us maintain the mesh resolution, and consequently the solution accuracy, near moving solid surfaces. The structural mechanics computations are based on the Kirchhoff-Love shell model. A set of special ST techniques is also used in the computations in conjunction with the ST-VMS method. The special techniques include using, in the ST flow computations, NURBS basis functions for the temporal representation of the prescribed part of the wing motion. The computational analysis presented includes comparing the lift and thrust generated with the wing motion fully and partially prescribed from the actual locust.en_US
dc.format.mimetypeapplication/pdfen_US
dc.identifier.citationMontel, Kenneth Keef. "Fluid-Structure Interaction Modeling of MAV Flapping-Wing Aerodynamics." (2015) Master’s Thesis, Rice University. <a href="https://hdl.handle.net/1911/88237">https://hdl.handle.net/1911/88237</a>.en_US
dc.identifier.urihttps://hdl.handle.net/1911/88237en_US
dc.language.isoengen_US
dc.rightsCopyright is held by the author, unless otherwise indicated. Permission to reuse, publish, or reproduce the work beyond the bounds of fair use or other exemptions to copyright law must be obtained from the copyright holder.en_US
dc.subjectMicro aerial vehicleen_US
dc.subjectBio-inspired flappingen_US
dc.subjectLocusten_US
dc.subjectFluid--Structure Interactionen_US
dc.subjectSpace--time techniquesen_US
dc.subjectBlock-Iterative Couplingen_US
dc.titleFluid-Structure Interaction Modeling of MAV Flapping-Wing Aerodynamicsen_US
dc.typeThesisen_US
dc.type.materialTexten_US
thesis.degree.departmentMechanical Engineeringen_US
thesis.degree.disciplineEngineeringen_US
thesis.degree.grantorRice Universityen_US
thesis.degree.levelMastersen_US
thesis.degree.nameMaster of Scienceen_US
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