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Towards a hybrid CFD platform for investigating aircraft trailing vortices
This dissertation outlines the development of a parallel 3D hybrid finite-volume- finite-difference solver. As motivation for such a scheme, the specific application area under consideration is modeling the trailing vortices shed from the wings of aircraft under transonic flight conditions. For this...
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| Format: | Thesis |
| Language: | English |
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Department of Mechanical Engineering
2018
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