Research graph
References from Numerical study on the influence of surface injection on the coupled thermal effects of ablative thermal protection systems under long-duration flight conditions. Local targets link to admitted publications; unresolved targets remain external evidence.
Unresolved reference
2019 · External reference
Combined thermal phenomena of hypersonic vehicle
10.1360/sspma2019-0060 · 2019 · External reference
Research progress of thermal protection technique by activemass injection for hypersonic vehicle
2022 · External reference
Research on the influence of surface injection on the aerodynamic heating of high-speed aircraft
2024 · External reference
Effects of wall mass injection on drag and heat reduction characteristics of high-speed flight vehicles
2023 · External 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 · 2024 · External 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 · 2025 · External reference
Enhanced ablation resistance of vinyl silicone rubber via liquid ceramicized precursor hyperbranched polycarbosilane modification
10.1016/j.cej.2025.167637 · 2025 · External reference
Unresolved reference
2019 · External reference
Survey of convective blockage for planetary entries
10.1016/j.actaastro.2012.06.016 · 2013 · External reference
Dynamics of pyrolysis gas in charring materials ablation
1998 · External reference
Gas-injection effects on wall heat flux and skin-friction of vehicles
2023 · External 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 · 2023 · External reference
Unresolved reference
2022 · External reference
Cocnjugate analysis of rocket nozzle ablation
2017 · External reference
Combined thermal phenomena issues of long endurance hypersonic vehicles
2020 · External reference
Research status of hypersonic vehicle fluid-thermal-solid coupling and software development
2017 · External reference
Valicdation process for blowing and transpiration-cooling in DPLR
2007 · External reference
Combined effects of mass addition and nose bluntness on boundary-layer transition
10.2514/3.5778 · 1970 · External reference
Numerical simulation and experimental analysis of ablation response behavior of silicone rubber based flexible ablative material
10.1016/j.compositesa.2025.109079 · 2025 · External reference
Multi-physics-coupled numerical simulation and experimental validation of ablation performance in silicone-rubber-based flexible thermal protection system
2025 · External reference
Aerothermal–heat transfer coupling calculation method based on whole ballistic iteration
10.1061/jaeeez.aseng-6113 · 2025 · External reference
Theory of stagnation point heat transfer in dissociated air
1958 · External reference
Solution strategy for thermal response of nonablating thermal protection systems at hypersonic speeds
1996 · External reference
A new data transfer method in fluid-thermal-structure coupling problems
2016 · External reference
The physical mechanism of convective heat transfer and control: synergy between velocity field and heat flow field
2000 · External reference
Survey of convective blockage for planetary entries
10.1016/j.actaastro.2012.06.016 · ExternalCitation · doi-reference
Enhanced ablation resistance of vinyl silicone rubber via liquid ceramicized precursor hyperbranched polycarbosilane modification
10.1016/j.cej.2025.167637 · ExternalCitation · doi-reference
Numerical simulation and experimental analysis of ablation response behavior of silicone rubber based flexible ablative material
10.1016/j.compositesa.2025.109079 · ExternalCitation · 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 · ExternalCitation · 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 · ExternalCitation · 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 · ExternalCitation · doi-reference
Aerothermal–heat transfer coupling calculation method based on whole ballistic iteration
10.1061/jaeeez.aseng-6113 · ExternalCitation · doi-reference
Combined thermal phenomena of hypersonic vehicle
10.1360/sspma2019-0060 · ExternalCitation · doi-reference
Combined effects of mass addition and nose bluntness on boundary-layer transition
10.2514/3.5778 · ExternalCitation · doi-reference
