Add to ORKGIn the arc heated facility LBK a transpiration cooling concept based on porous CMC material was qualified for application in external hypersonic flow, in particular for atmospheric entry. The experimental setup allowed a direct comparison of the thermal behaviour of transpiration cooling to a well-qualified passive thermal protection technology. Tests were performed for different coolants at various flow rates in order to identify the influence on cooling efficiency. Nitrogen, argon and helium were used as coolants. It was found that for a given configuration there is an optimal coolant flow rate for each coolant. These optimal coolant flow rates could be identified and compared for all coolants used
At the German Aerospace Center (DLR), a possible solution for handling extreme aerothermodynamic hea...
An investigation of transpiration cooling has been conducted in the preflight jet of the Langley Pil...
The thermal management of air-breathing vehicles presents formidable challenges. The high dynamic pr...
Specific parts of re-entry vehicles are exposed to severe conditions. Thereby, the material’s capabi...
The extremely high heat loads within a Scramjet combustor require the use of high-temperature materi...
The extremely high heat loads within a Scramjet combustor require the use of high-temperature materi...
The extremely high heat loads within a Scramjet combustor require the use of high-temperature materi...
The extremely high heat loads within a Scramjet combustor require the use of high-temperature materi...
This paper presents results of a system study of transpiration cooled thermal protection systems for...
This paper presents results of a system study of transpiration cooled thermal protection systems for...
As a promising and efficient active cooling method, double layer transpiration cooling is introduced...
One of the main challenges for scramjet propulsion systems is the efficient and sufficient cooling o...
In a preliminary feasibility study, transpiration cooling in the supersonic flow of a conical laval ...
High speed sustained atmospheric flight creates high thermal loads at the tip, leading edges, intake...
Transpiration cooling technique is one of the most promising candidates as the next‐generation TPS ‐...
At the German Aerospace Center (DLR), a possible solution for handling extreme aerothermodynamic hea...
An investigation of transpiration cooling has been conducted in the preflight jet of the Langley Pil...
The thermal management of air-breathing vehicles presents formidable challenges. The high dynamic pr...
Specific parts of re-entry vehicles are exposed to severe conditions. Thereby, the material’s capabi...
The extremely high heat loads within a Scramjet combustor require the use of high-temperature materi...
The extremely high heat loads within a Scramjet combustor require the use of high-temperature materi...
The extremely high heat loads within a Scramjet combustor require the use of high-temperature materi...
The extremely high heat loads within a Scramjet combustor require the use of high-temperature materi...
This paper presents results of a system study of transpiration cooled thermal protection systems for...
This paper presents results of a system study of transpiration cooled thermal protection systems for...
As a promising and efficient active cooling method, double layer transpiration cooling is introduced...
One of the main challenges for scramjet propulsion systems is the efficient and sufficient cooling o...
In a preliminary feasibility study, transpiration cooling in the supersonic flow of a conical laval ...
High speed sustained atmospheric flight creates high thermal loads at the tip, leading edges, intake...
Transpiration cooling technique is one of the most promising candidates as the next‐generation TPS ‐...
At the German Aerospace Center (DLR), a possible solution for handling extreme aerothermodynamic hea...
An investigation of transpiration cooling has been conducted in the preflight jet of the Langley Pil...
The thermal management of air-breathing vehicles presents formidable challenges. The high dynamic pr...