A Conformal Mapping Grid Generation Method for Modeling High-Fidelity Aeroelastic Simulations

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dc.contributorCizmas, Paul
dc.creatorWorley, Gregory
dc.date.accessioned2010-07-15T00:16:26Z
dc.date.accessioned2010-07-23T21:47:12Z
dc.date.accessioned2017-04-07T19:57:21Z
dc.date.available2010-07-15T00:16:26Z
dc.date.available2010-07-23T21:47:12Z
dc.date.available2017-04-07T19:57:21Z
dc.date.created2010-05
dc.date.issued2010-07-14
dc.description.abstractThis work presents a method for building a three-dimensional mesh from two- dimensional topologically identical layers, for use in aeroelastic simulations. The method allows modeling of large deformations of the wing in both the span direction and deformations in the cord of the wing. In addition, the method allows for the modeling of wings attached to fuselages. The mesh created is a hybrid mesh, which allows cell clustering in the viscous region. The generated mesh is high quality and allows capturing of nonlinear uid structure interactions in the form of limit cycle oscillation.
dc.identifier.urihttp://hdl.handle.net/1969.1/ETD-TAMU-2010-05-7747
dc.language.isoeng
dc.subjectAeroelasticity
dc.subjectunsteady aerodynamics
dc.subjectcomputational fl uid dynamics
dc.subjectgrid generation
dc.subjectconformal mapping
dc.subjectlimit cycle oscillation
dc.subjectnonlinear
dc.titleA Conformal Mapping Grid Generation Method for Modeling High-Fidelity Aeroelastic Simulations
dc.typeBook
dc.typeThesis

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