Assessment of heat flux prediction capabilities of residual distribution method: application to atmospheric entry problems

JG Mena, R Pepe, A Lani… - … in Computational Physics, 2015 - cambridge.org
In the present contribution we evaluate the heat flux prediction capabilities of second-order
accurate Residual Distribution (RD) methods in the context of atmospheric (re-) entry …

[PDF][PDF] An effective treatment of numerical shock wave instabilities with residual distribution schemes: Application to hypersonic nonequilibrium flows around blunt …

JG Mena, A Lani, K Sermeus… - … European Symposium on …, 2011 - researchgate.net
In the present contribution the issue of simulating hypersonic flows by means of Residual
Distribution Schemes is discussed. In particular, this discretization technique is briefly …

An enthalpy‐preserving shock‐capturing term for residual distribution schemes

J Garicano‐Mena, G Degrez - International Journal for …, 2018 - Wiley Online Library
In this contribution, we investigate strategies to perform shock‐capturing computation of
steady hypersonic flow fields by means of residual distribution schemes. The ultimate …

[PDF][PDF] On the computation of heat flux in hypersonic flows using Residual Distribution Schemes

JG Mena - 2014 - dipot.ulb.ac.be
In this dissertation the heat flux prediction capabilities of Residual Distribution (RD) schemes
for hypersonic flow fields are investigated. Two canonical configurations are considered: the …

[PDF][PDF] Assessment of Heat Flux Prediction Capabilities of Residual Distribution Method: Application to Atmospheric Entry Problems

H Deconinck - 2015 - global-sci.com
In the present contribution we evaluate the heat flux prediction capabilities of second-order
accurate Residual Distribution (RD) methods in the context of atmospheric (re-) entry …

[PDF][PDF] A Conservative Linearization Procedure for Simulating Hypersonic Nonequilibrium Flows with Residual Distribution Schemes

JG Mena, A Lani, H Deconinck - researchgate.net
In this contribution, a linearization procedure guaranteeing conservation across the strong
shock waves typical of hypersonic flows is adapted for a multidimensional upwind Residual …