Computational simulations of near-continuum gas flow using Navier-Stokes-Fourier equations with slip and jump conditions based on the modal discontinuous Galerkin method
Abstract Blunt-body configurations are the most common geometries adopted for non-lifting re-entry vehicles. Hypersonic re-entry vehicles experience different flow regimes during flight due to drastic changes in atmospheric density. The conventional Navier-Stokes-Fourier equations with no-slip and n...
Main Authors: | T. Chourushi, A. Rahimi, S. Singh, R. S. Myong |
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Format: | Article |
Language: | English |
Published: |
SpringerOpen
2020-04-01
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Series: | Advances in Aerodynamics |
Subjects: | |
Online Access: | http://link.springer.com/article/10.1186/s42774-020-00032-z |
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