High-order shock-fitting methods for direct numerical simulation of hypersonic flow with chemical and thermal nonequilibrium
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Publication:414016
DOI10.1016/j.jcp.2011.08.001zbMath1337.76041OpenAlexW2072979773MaRDI QIDQ414016
Publication date: 8 May 2012
Published in: Journal of Computational Physics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.jcp.2011.08.001
Related Items (11)
DeepM\&Mnet for hypersonics: predicting the coupled flow and finite-rate chemistry behind a normal shock using neural-network approximation of operators ⋮ Energy relaxation approximation for compressible multicomponent flows in thermal nonequilibrium ⋮ Computational simulations of microscale shock-vortex interaction using a mixed discontinuous Galerkin method ⋮ A method for the direct numerical simulation of hypersonic boundary-layer instability with finite-rate chemistry ⋮ Cross-flow vortices and their secondary instabilities in hypersonic and high-enthalpy boundary layers ⋮ A shock-fitting technique for cell-centered finite volume methods on unstructured dynamic meshes ⋮ Convergence acceleration for high-order shock-fitting methods in hypersonic flow applications with efficient implicit time-stepping schemes ⋮ New very high-order upwind multi-layer compact (MLC) schemes with spectral-like resolution for flow simulations ⋮ Extrapolated shock tracking: bridging shock-fitting and embedded boundary methods ⋮ Numerical simulation of shock-disturbances interaction in high-speed compressible inviscid flow over a blunt nose using weighted essentially non-oscillatory scheme ⋮ A novel combination of mathematical modelling approaches for simulating nearly hypersonic, viscous, reacting magnetogasdynamic flows
Uses Software
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