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...

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Bibliographic Details
Main Authors: T. Chourushi, A. Rahimi, S. Singh, R. S. Myong
Format: Article
Language:English
Published: SpringerOpen 2020-04-01
Series:Advances in Aerodynamics
Subjects:
Online Access:http://link.springer.com/article/10.1186/s42774-020-00032-z