Summary
This work focuses on the numerical simulation of laminar, three-dimensional, symmetric corner flows in the hypersonic regime. For this purpose an algorithm based on a Finite-Volume-Method with cell vertex approach and explicit time integration is used. Different Upwind-Splitting methods have been implemented with emphasis on differences among these methods regarding the overall quality of the corresponding results. A description of the schemes is presented and the results are compared with experimental data as well as with results from other authors for two different corner flow problems.
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© 1999 Springer Fachmedien Wiesbaden
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van Keuk, J., Ballmann, J. (1999). Numerical Simulation of Laminar Symmetric Corner Flows in the Hypersonic Regime. In: Nitsche, W., Heinemann, HJ., Hilbig, R. (eds) New Results in Numerical and Experimental Fluid Mechanics II. Notes on Numerical Fluid Mechanics (NNFM), vol 72. Vieweg+Teubner Verlag, Wiesbaden. https://doi.org/10.1007/978-3-663-10901-3_33
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DOI: https://doi.org/10.1007/978-3-663-10901-3_33
Publisher Name: Vieweg+Teubner Verlag, Wiesbaden
Print ISBN: 978-3-663-10903-7
Online ISBN: 978-3-663-10901-3
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