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A Multiscale Flow-Material Coupling Study of Silicone Rubber-Based Insulation in a Dual-Inlet SDR Combustor: Regionalized Thermo-Mechanical Loading and Melt-Redistribution-Controlled Ablation

https://doi.org/10.2139/ssrn.6958661
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Ceramifiable Flame-Retarded Silicone Rubber Composites Based on Novel Phosphorus/Nitrogen/Silicon-Containing Flame Retardants
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Performance Analysis of a Ducted Rocket Under Various Flight Conditions
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The numerical computation of turbulent flows
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Radiative properties of alumina/aluminum particles and influence on radiative heat transfer in solid rocket motor
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Analysis of combustion modes in a cavity based scramjet
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Zero-ablative-recession nanoporous silicone composites with exceptional mechanical-thermal stability for reusable thermal protection system
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3D shape-stable temperature-regulated macro-encapsulated phase change material: KAl(SO4)2·12H2O-C2H2O4·2H2O-CO(NH2)2 eutectic/polyurethane foam as core and carbon modified silicone resin as shell
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Ablative properties, thermal stability, and compressive behaviour of hybrid silica phenolic ablative composites.
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Modeling and validation of ablative thermal response combined with microscopic heat transfer for porous ablative materials
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Unified Analysis of Internal Flowfield in an Integrated Rocket Ramjet Engine. I: Transition from Rocket Booster to Ramjet Sustainer
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Numerical simulation of particle erosion in the internal flow field of solid rocket motor nozzle using Rocstar
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Investigation of the effects of alumina particle phase transition on internal flow field and engine performance in solid rocket motors
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Numerical analysis of ablative behavior of silicone resin coated carbon fabric
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Failure Characterization of Silicone Rubber in Corrosive Environments Based on Leakage Current Characteristics
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Mechanical Erosion Investigation in Solid Rocket Motor Nozzle Through Droplet Breakup and Surface Tension Influence
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Exploration of a new affordable thermal protection system utilizing 2.5D silica/polysiloxane composite
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Reassessment of the scale-determining equation for advanced turbulence models
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Two-equation eddy-viscosity turbulence models for engineering applications
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Research on Ablation Device Suitable for Thermal Protection System of Solid Rocket Ramjet
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Supersonic Combustion Mode Analysis of a Cavity Based Scramjet
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Improving the Ablation Properties of Liquid Silicone Rubber Composites by Incorporating Hexaphenoxycyclotriphosphonitrile
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Ceramifiable Silicone Rubber Composites with Enhanced Self-Supporting and Ceramifiable Properties
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