Steerneman, B.J. (2007) An efficient semi-implicit time integration method for extra large eddy simulations. Master's Thesis / Essay, Mathematics.
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Abstract
The use of Computational Fluid Dynamics (CFD) is a common factor in the technical design industry these days. For example, the design of rockets, airplanes and Formula 1 cars would not be the same without CFD. When only the averaged drag coefficient or the averaged forces are needed, time independent simulations are sufficient. However, for a lot of applications knowing only the averaged values is not sufficient. One can think of the unsteady flow that comes from the central core of a space launcher which creates unsteady forces on its nozzle during take-off. Knowing only the averaged values makes it impossible to create a cost effective space launcher which is strong enough to withstand those unsteady forces. For those problems time dependent computations are necessary.
| Item Type: | Thesis (Master's Thesis / Essay) |
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| Degree programme: | Mathematics |
| Thesis type: | Master's Thesis / Essay |
| Language: | English |
| Date Deposited: | 15 Feb 2018 07:28 |
| Last Modified: | 15 Feb 2018 07:28 |
| URI: | https://fse.studenttheses.ub.rug.nl/id/eprint/8374 |
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