A mathematical model of the thermochemical destruction of carbon fiber-reinforced plastic in the presence of surface roughness and composite ablation is refined based on known theoretical results. It is shown that mass loss through rough surface ambiguously influences the intensity of heat exchange processes in thermal protective material. Results of numerical calculations are compared with known data
Carbon/carbon composites are usually used as a thermal protection material in the nose cap and leadi...
A coupled thermomechanical analysis of composite structures in pyrolysis and ablation environments i...
Durant la phase de descente d'un véhicule de rentrée atmosphérique, des pressions et flux de chaleur...
A mathematical model of the thermochemical destruction of carbon fiber-reinforced plastic in the pre...
The thermochemical destruction of a carbon fiber-reinforced polymer when affected by a high enthalpy...
A numerical analysis of the nonstationary heat and mass exchange in the heat-resistant composite mat...
Roughness of heat-shield materials has been studied in the frame of aerodynamics and the laminar-tur...
Surface ablation and in-depth temperature distribution of the charring material are the key properti...
This article derives and provides a theoretical analysis for the mechanical erosion of carbon-base m...
peer reviewedHigh-fidelity models have been developed in the recent years to predict the response of...
Because of their unique ablative properties, many carbon-based heterogeneous materials are used as c...
This work aims to explain and model the complex behavior of carbon-carbon composites during ablation...
This paper is concerned with modeling of ablation behavior of carbon-carbon composites used in hot s...
The TPS (Thermal Protection System) is a subsystem providing protection and isolation from aerodynam...
International audienceBecause of their unique ablative properties, many carbon-based heterogeneous m...
Carbon/carbon composites are usually used as a thermal protection material in the nose cap and leadi...
A coupled thermomechanical analysis of composite structures in pyrolysis and ablation environments i...
Durant la phase de descente d'un véhicule de rentrée atmosphérique, des pressions et flux de chaleur...
A mathematical model of the thermochemical destruction of carbon fiber-reinforced plastic in the pre...
The thermochemical destruction of a carbon fiber-reinforced polymer when affected by a high enthalpy...
A numerical analysis of the nonstationary heat and mass exchange in the heat-resistant composite mat...
Roughness of heat-shield materials has been studied in the frame of aerodynamics and the laminar-tur...
Surface ablation and in-depth temperature distribution of the charring material are the key properti...
This article derives and provides a theoretical analysis for the mechanical erosion of carbon-base m...
peer reviewedHigh-fidelity models have been developed in the recent years to predict the response of...
Because of their unique ablative properties, many carbon-based heterogeneous materials are used as c...
This work aims to explain and model the complex behavior of carbon-carbon composites during ablation...
This paper is concerned with modeling of ablation behavior of carbon-carbon composites used in hot s...
The TPS (Thermal Protection System) is a subsystem providing protection and isolation from aerodynam...
International audienceBecause of their unique ablative properties, many carbon-based heterogeneous m...
Carbon/carbon composites are usually used as a thermal protection material in the nose cap and leadi...
A coupled thermomechanical analysis of composite structures in pyrolysis and ablation environments i...
Durant la phase de descente d'un véhicule de rentrée atmosphérique, des pressions et flux de chaleur...