Detailed chemical equilibrium model for porous ablative materials
Authors:
- Jean LachaudJLJean Lachaud
- Tom van EekelenTETom van Eekelen
- James B. ScogginsJSJames B. Scoggins
- Thierry E. MaginTMThierry E. Magin
- Nagi N. MansourNMNagi N. Mansour
- 1 November 2015
- journal article
- research article
- Published by Elsevier in International Journal of Heat and Mass Transfer
- Vol. 90, 1034-1045
Abstract
No abstract availableKeywords
Funding Information
- NASA’s Fundamental Aeronautic Program Hypersonics NRA (NNX12AG47A)
- European Research Council (#259354)
This publication has 17 references indexed in Scilit:
- Numerical study of iso-Q sample geometric effects on charring ablative materialsInternational Journal of Heat and Mass Transfer, 2015
- Mars Science Laboratory Heat Shield Aerothermodynamics: Design and ReconstructionJournal of Spacecraft and Rockets, 2014
- Porous-Material Analysis Toolbox Based on OpenFOAM and ApplicationsJournal of Thermophysics and Heat Transfer, 2014
- Postflight Thermal Protection System Analysis of Hayabusa Reentry CapsuleJournal of Spacecraft and Rockets, 2014
- Multiscale Approach to Ablation Modeling of Phenolic Impregnated Carbon AblatorsJournal of Spacecraft and Rockets, 2010
- Ablation and Thermal Response Property Model Validation for Phenolic Impregnated Carbon AblatorJournal of Spacecraft and Rockets, 2010
- Erratum on "Performance of a Low Density Ablative Heat Shield Material"Journal of Spacecraft and Rockets, 2008
- Analytical modeling of the steady state ablation of a 3D C/C compositeInternational Journal of Heat and Mass Transfer, 2008
- Quasi-steady solutions for the ablation of charring materialsInternational Journal of Heat and Mass Transfer, 2007
- Ablation of carbon-based materials: Investigation of roughness set-up from heterogeneous reactionsInternational Journal of Heat and Mass Transfer, 2005