We introduce an immersed high-order discontinuous Galerkin method for solving the compressible Navier-Stokes equations on non-boundary-fitted meshes. The flow equations are discretised with a mixed discontinuous Galerkin formulation and are advanced in time with an explicit time marching scheme. The discretisation meshes may contain simplicial (triangular or tetrahedral) elements of different sizes and need not be structured. On the discretisation mesh, the fluid domain boundary is represented with an implicit signed distance function. The cut-elements partially covered by the solid domain are integrated after tessellation with the marching triangle or tetrahedra algorithms. Two alternative techniques are introduced to overcome the excessive stable time step restrictions imposed by cut-elements. In the first approach, the cut-basis functions are replaced with the extrapolated basis functions from the nearest largest element. In the second approach, the cut-basis functions are simply scaled proportionally to the fraction of the cut-element covered by the solid. To achieve high-order accuracy, additional nodes are introduced on the element faces abutting the solid boundary. Subsequently, the faces are curved by projecting the introduced nodes to the boundary. The proposed approach is verified and validated with several two- and three-dimensional subsonic and hypersonic low Reynolds number flow applications, including the flow over a cylinder, a space capsule, and an aerospace vehicle.
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French Aerosp Lab, ONERA, F-92320 Chatillon, FranceFrench Aerosp Lab, ONERA, F-92320 Chatillon, France
Renac, Florent
Gerald, Sophie
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French Aerosp Lab, ONERA, F-92320 Chatillon, France
UPMC Univ Paris 06, UMR 7598, Lab Jacques Louis Lions, F-75005 Paris, FranceFrench Aerosp Lab, ONERA, F-92320 Chatillon, France
Gerald, Sophie
Marmignon, Claude
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French Aerosp Lab, ONERA, F-92320 Chatillon, FranceFrench Aerosp Lab, ONERA, F-92320 Chatillon, France
Marmignon, Claude
Coquel, Frederic
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机构:
Ecole Polytech, CMAP CNRS UMR 7641, F-91128 Palaiseau, FranceFrench Aerosp Lab, ONERA, F-92320 Chatillon, France
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College of Aerospace Engineering,Nanjing University of Aeronautics and AstronauticsCollege of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics
Sun Qiang
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Lyu Hongqiang
Wu Yizhao
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College of Aerospace Engineering,Nanjing University of Aeronautics and AstronauticsCollege of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics
机构:
Univ Tokyo, Dept Comp Sci, Tokyo 1138656, Japan
Fukushima Univ, Informat Network Ctr, Fukushima, Fukushima 9601296, JapanUniv Tokyo, Dept Comp Sci, Tokyo 1138656, Japan