par Schrooyen, Pierre;Hillewaert, Koen;Magin, Thierry 
;Chatelain, Philippe
Référence 21st AIAA Computational Fluid Dynamics Conference(21: 2013-06-24), American Institute of Aeronautics and Astronautics Inc
Publication Publié, 2013
;Chatelain, PhilippeRéférence 21st AIAA Computational Fluid Dynamics Conference(21: 2013-06-24), American Institute of Aeronautics and Astronautics Inc
Publication Publié, 2013
Publication dans des actes
| Résumé : | The interaction between the mechanisms of ablation and boundary layer transition is one of the phenomena that leads to diffculties in heat-flux prediction during atmospheric entries. The objective of this work is to develop a computational tool based on a high- order discontinuous Galerkin method (DGM), that simulates and models the flow and wall phenomena in a unified approach. As a first step, a one-dimensional code has been developed for the in-depth thermal response of ablative materials. This paper demonstrates the capability of DGM for discretizing the highly-nonlinear problem equations, discusses specificities of the method to ensure stability and illustrates the subsequent validation. A sharp interface method is proposed to face the challenges of recession front modeling. |
