Porous-material analysis toolbox based on OpenFOAM and applications

J Lachaud, NN Mansour - Journal of Thermophysics and Heat Transfer, 2014 - arc.aiaa.org
The Porous-material Analysis Toolbox based on OpenFOAM is a fully portable OpenFOAM
library. It is implemented to test innovative multiscale physics-based models for reacting …

Numerical modeling of ablation heat transfer

ME Ewing, TS Laker, DT Walker - Journal of Thermophysics and Heat …, 2013 - arc.aiaa.org
A unique numerical method has been developed for solving one-dimensional ablation heat
transfer problems. This paper provides a comprehensive description of the method, along …

CHyPS: A high-order material response solver for ablative thermal protection systems

RM Chiodi, KA Stephani, M Panesi… - AIAA SCITECH 2022 …, 2022 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2022-1501. vid Reentry and hypersonic
vehicles are exposed to high temperatures during flight that require the use of thermal …

Two-dimensional modeling of ablation and pyrolysis with application to rocket nozzles

PG Cross, ID Boyd - Journal of Spacecraft and Rockets, 2017 - arc.aiaa.org
A new two-dimensional ablation analysis code (MOPAR-MD) capable of modeling
pyrolyzing thermal protection system materials is presented. Favorable agreement with …

Ablation Test-Case Series# 2. Numerical Simulation of Ablative-Material Response: Code and Model Comparisons

JR Lachaud, A Martin, T van Eekelen, I Cozmuta - 2012 - uknowledge.uky.edu
This test-case series on the numerical simulation of the response of ablative-materials really
started out of pure curiosity. Code developers and users were curious to see" how the codes …

Two-way coupled simulations of stagnation-point ablation with transient material response

P Schrooyen, A Turchi, K Hillewaert, P Chatelain… - International Journal of …, 2018 - Elsevier
Ablative materials are extensively used in aerospace applications to protect the integrity of
the spacecraft during atmospheric entry. Both thermal and mechanical stresses have to be …

Modeling instrumented test articles for Plasmatron X aerothermal environment

S Oruganti, S Kumar, V Le Maout, L Capponi… - AIAA Aviation 2023 …, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-3327. vid This work discusses the
ablative response of thermal protection system materials when exposed to aerothermal …

[PDF][PDF] Numerical simulation of aerothermal flows through ablative thermal protection systems

P Schrooyen - 2015 - core.ac.uk
The exploration programs of our solar system involve the design of manned or unmanned
spacecraft that enter a planet atmosphere at hypersonic velocity. After the successful …

An implicit coupling framework for numerical simulations between hypersonic nonequilibrium flows and thermal responses of charring materials in the presence of …

J Zhang, C Nie, J Cai, S Pan - Aerospace Science and Technology, 2024 - Elsevier
An implicit coupling framework for hypersonic nonequilibrium flows and material thermal
responses is proposed for numerical simulations of ablative thermal protection materials …

Evaluation of numerical ablation model for charring composites

W Li, J Zhang, GD Fang, WJ Li, J Liang… - Science China …, 2019 - Springer
Charring composites are widely used in the thermal protection system (TPS) to consume the
intense aerodynamic heating during vehicle reentry. The ablation and thermal responses for …