Abstract
Qi You, Zhenxun Gao, Binxian Shen, Lei Zeng, Chongwen Jiang
Abstract
Authors
Institutions
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Unresolved referenced work
2019
Combined thermal phenomena of hypersonic vehicle
10.1360/sspma2019-0060 · 2019
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Constructing layered structure improves thermal protection performance of silicone rubber-based composites under coupled mechanical-thermal-oxidative conditions
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Provenance
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Aerothermal–heat transfer coupling calculation method based on whole ballistic iteration
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Numerical simulation and experimental analysis of ablation response behavior of silicone rubber based flexible ablative material
10.1016/j.compositesa.2025.109079 · doi-reference
Combined effects of mass addition and nose bluntness on boundary-layer transition
10.2514/3.5778 · doi-reference
Heat transfer and pyrolysis gas flow characteristics of light-weight ablative thermal protection system in the blunt body
10.1016/j.ijthermalsci.2022.108122 · doi-reference
Survey of convective blockage for planetary entries
10.1016/j.actaastro.2012.06.016 · doi-reference
Enhanced ablation resistance of vinyl silicone rubber via liquid ceramicized precursor hyperbranched polycarbosilane modification
10.1016/j.cej.2025.167637 · doi-reference
Constructing layered structure improves thermal protection performance of silicone rubber-based composites under coupled mechanical-thermal-oxidative conditions
10.1016/j.conbuildmat.2025.141327 · doi-reference
Incorporating metal oxides to significantly improve the ablative performance of silicone rubber-based composites at 10% tensile strain rate under coupled thermal-mechanical-oxidative conditions
10.1021/acs.iecr.4c03552 · doi-reference
Combined thermal phenomena of hypersonic vehicle
10.1360/sspma2019-0060 · doi-reference