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• W4384993183 abstract "High heat fluxes generated by aerodynamic heating or rocket propellant burning create a high demand for the use Thermal Protection Systems (TPS) to prevent damage or malfunctioning in payloads and rocket parts. Thermophysical and ablative properties of TPS materials are needed for their design, but are commonly unavailable or difficult to access experimentally. Besides, materials present different responses to high heat fluxes according to their composition and manufacturing process. Inverse heat transfer problems were initially studied to determine not known variables in thermal behavior of space vehicles and have proven to reach reliable properties values of ablative materials. This work applies an already validated methodology, using the Markov chain Monte Carlo (MCMC) method applied to a lumped physical model of ablation, to determine thermophysical and ablation properties of different composite materials starting from arc-jet ablation results. The direct problem with a more refined mesh and the obtained values of these properties was used and the numerical results were compared to the experiments, presenting good agreement and resulting in lower rms values, when compared to original values extracted from literature." @default.
• W4384993183 created "2023-07-22" @default.
• W4384993183 creator A5025409291 @default.
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• W4384993183 date "2023-10-01" @default.
• W4384993183 modified "2023-09-24" @default.
• W4384993183 title "Application of the Markov chain Monte Carlo analysis through a lumped model in ablation test results of ablative and reradiative materials" @default.
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• W4384993183 doi "https://doi.org/10.1016/j.icheatmasstransfer.2023.106955" @default.
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