Effect of Thermal Ablation at the Fluid-Solid Interface of a Hypersonic Reentry Vehicle in Rarefied Flow Regime
DOI10.1080/10618562.2021.2017900zbMath1487.76051OpenAlexW4200391113MaRDI QIDQ5075247
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Publication date: 10 May 2022
Published in: International Journal of Computational Fluid Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1080/10618562.2021.2017900
convective heat transferreentry vehiclethermal protection systemablative materialconjugate thermal analysisdirect simulation Monte Carlo flow solver
Stochastic analysis applied to problems in fluid mechanics (76M35) Rarefied gas flows, Boltzmann equation in fluid mechanics (76P05) Hypersonic flows (76K05) Diffusive and convective heat and mass transfer, heat flow (80A19)
Uses Software
Cites Work
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