Proceedings of the VII European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS Congress 2016) 2016
DOI: 10.7712/100016.1846.8406
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Addressing the Challenges of Implementation of High-Order Finite-Volume Schemes for Atmospheric Dynamics on Unstructured Meshes

Abstract: Abstract. The solution of the non-hydrostatic compressible Euler equations using Weighted Es

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Cited by 10 publications
(6 citation statements)
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“…To avoid the growth of instabilities in the numerical solution, we may add a small artificial viscosity. However, as already discussed in [102,103,105], this leads to a smoothness of the boundary of the bubble, that is affected by numerical dissipation. Figure 12 shows the results obtained at time instants t ∈ {600, 700, 800, 900}s using a constant artificial viscosity with µ = 10 −6 and a very coarse primal mesh composed of only 5172 triangles.…”
Section: Warm Bubble In Two Space Dimensionsmentioning
confidence: 88%
See 1 more Smart Citation
“…To avoid the growth of instabilities in the numerical solution, we may add a small artificial viscosity. However, as already discussed in [102,103,105], this leads to a smoothness of the boundary of the bubble, that is affected by numerical dissipation. Figure 12 shows the results obtained at time instants t ∈ {600, 700, 800, 900}s using a constant artificial viscosity with µ = 10 −6 and a very coarse primal mesh composed of only 5172 triangles.…”
Section: Warm Bubble In Two Space Dimensionsmentioning
confidence: 88%
“…We now extend the warm bubble test to a three-dimensional domain, following the setup described in [105,104]. To this end, we define the computational domain Ω = [0, 1] × [0, 1] × [0, 1.5] km.…”
Section: Warm Bubble In Three Space Dimensionsmentioning
confidence: 99%
“…The present polynomial reconstruction is based upon the approaches of [53,63], that have been applied to smooth and discontinuous flow problems [2][3][4][5]20,46,49,50,57,[59][60][61][62][64][65][66][67], and only the key-components will be presented herein and the reader is referred to [53,63] for further details. For the reconstruction, a transformation from physical space to a reference space as introduced by Dumbser et al [16,17] is employed to reduce the scaling effects that occur at unstructured meshes consisting of elements of different shape and size.…”
Section: Reconstructionmentioning
confidence: 99%
“…The reconstruction algorithm used is based upon the approaches [2,3,11,35], that have been applied to smooth and discontinuous flow problems [22,[38][39][40][41][42][43][44][45][46][47] and only key-components will be presented herein, since the focus is towards the stencil selection algorithms and the reader is referred to [2,3,35] for further details.…”
Section: Spatial Discretisationmentioning
confidence: 99%