This 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.
| Identifer | oai:union.ndltd.org:tamu.edu/oai:repository.tamu.edu:1969.1/ETD-TAMU-2010-05-7747 |
| Date | 2010 May 1900 |
| Creators | Worley, Gregory |
| Contributors | Cizmas, Paul |
| Source Sets | Texas A and M University |
| Language | English |
| Detected Language | English |
| Type | Book, Thesis, Electronic Thesis, text |
| Format | application/pdf |
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