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dc.contributor.advisorRaúl Radovitzky.en_US
dc.contributor.authorTam, Daniel See Wai, 1980-en_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2005-06-02T18:52:24Z
dc.date.available2005-06-02T18:52:24Z
dc.date.copyright2004en_US
dc.date.issued2004en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/17838
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004.en_US
dc.descriptionIncludes bibliographical references (p. 89-94).en_US
dc.description.abstractThe design of future light aerospace structures will require numerical tools to accurately describe the strongly coupled dynamics of the interactions between a light structure and a flow surrounding it. Specific examples include inflatable structures and parachutes used as deceleration devices during planet entry. In this work, an algorithm for simulating the solid-fluid interactions of a highly-deformable open shell structure and a compressible fluid flow is presented. The main objective is to extend the algorithm previously presented by the authors to the case of open shell structures immersed in a fluid. For simplicity, we restrict our attention to the two-dimensional case. The computational strategy is based on combining an Eulerian finite volume formulation for the fluid and a Lagrangian formulation for the structural response. The coupling between the fluid and the solid response is achieved via a novel approach based on extrapolation and velocity reconstruction aided by level sets. The accuracy of the proposed approach is verified against exact solutions of supersonic flow past a rigid flat plate. The numerical results reproduce all the details of the flow field, including the-very important-forces on the structure. The versatility of the proposed coupling algorithm is demonstrated in simulations of supersonic flow past a highly-deformable infinite plate.en_US
dc.description.statementofresponsibilityby Daniel See Wai Tam.en_US
dc.format.extent94 p.en_US
dc.format.extent4337782 bytes
dc.format.extent4346802 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582
dc.subjectAeronautics and Astronautics.en_US
dc.titleA two-dimensional fluid-structure coupling algorithm for the interaction of high-speed flows with open shellsen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc56570723en_US


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