Abstract The active cooling of aerospace structures can be performed by the use of porous materials. It requires characterizing its permeability to predict the cooling effi-ciency by means of Computational Fluid Dynamics codes. The Darcian term is generally deduced experimentally from a relationship between the mass flow rate and the pressure drop through the porous media. Due to thermo-chemical process involved in the cooling, the permeability can change. It is currently not possible with common techniques to determine these variations during the flight. This paper presents a novel approach taking advantage of well known flow behaviour in chemical reactor engineering in order to propose a real-time in situ quantification of the Darcian per...
Porous ultra-high-temperature ceramics (UHTCs) are a candidate group of materials for transpiration ...
Porous ultra-high-temperature ceramics (UHTCs) are a candidate group of materials for transpiration ...
This paper presents a methodology to infer the internal heat transfer characteristics of a porous Ul...
The thermal load protection of hypersonic and space vehicle structures can be achieved by either pas...
cited By (since 1996) 0International audienceLarge heat load are encountered in hypersonic and space...
The Non-Integer System Identification (NISI) method is an useful tool for the determination of surfa...
This paper presents a novel experimental technique where infrared thermography is employed to direct...
The Non-Integer System Identification (NISI) method is an useful tool for the determination of surfa...
The thermal load protection of hypersonic and space vehicle structures can be achieved by either pas...
This paper experimentally examines the internal and external flow characteristics of porous zirconiu...
Advances in space propulsion require the use of new materials. The Institute of Space Propulsion at ...
This paper presents a novel experimental technique where infra-red thermography is employed to direc...
Rocket combustion chambers are subject to extremely high thermal loads. To protect the chamber walls...
Transpiration cooling in combination with permeable ceramic-matrix composite materials is an innova...
Hot spots have been experimentally observed in porous materials in several applications as volumetri...
Porous ultra-high-temperature ceramics (UHTCs) are a candidate group of materials for transpiration ...
Porous ultra-high-temperature ceramics (UHTCs) are a candidate group of materials for transpiration ...
This paper presents a methodology to infer the internal heat transfer characteristics of a porous Ul...
The thermal load protection of hypersonic and space vehicle structures can be achieved by either pas...
cited By (since 1996) 0International audienceLarge heat load are encountered in hypersonic and space...
The Non-Integer System Identification (NISI) method is an useful tool for the determination of surfa...
This paper presents a novel experimental technique where infrared thermography is employed to direct...
The Non-Integer System Identification (NISI) method is an useful tool for the determination of surfa...
The thermal load protection of hypersonic and space vehicle structures can be achieved by either pas...
This paper experimentally examines the internal and external flow characteristics of porous zirconiu...
Advances in space propulsion require the use of new materials. The Institute of Space Propulsion at ...
This paper presents a novel experimental technique where infra-red thermography is employed to direc...
Rocket combustion chambers are subject to extremely high thermal loads. To protect the chamber walls...
Transpiration cooling in combination with permeable ceramic-matrix composite materials is an innova...
Hot spots have been experimentally observed in porous materials in several applications as volumetri...
Porous ultra-high-temperature ceramics (UHTCs) are a candidate group of materials for transpiration ...
Porous ultra-high-temperature ceramics (UHTCs) are a candidate group of materials for transpiration ...
This paper presents a methodology to infer the internal heat transfer characteristics of a porous Ul...