Novel heat flux controlled surface cooling for hypersonic flight

This paper presents a new method in theory and experiment to adjust the transpiration cooling based on the actual measured heat flux. This is particularly useful in extreme heating environments, e.g. atmospheric entry flight or combustion chamber applications. In such environments, usually cooling i...

Descripción completa

Detalles Bibliográficos
Autores principales: Hufgard, Fabian, Duernhofer, Christian, Fasoulas, Stefanos, Loehle, Stefan
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Nature Publishing Group UK 2023
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10421943/
https://www.ncbi.nlm.nih.gov/pubmed/37568038
http://dx.doi.org/10.1038/s41598-023-40281-8

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10421943/
https://www.ncbi.nlm.nih.gov/pubmed/37568038
http://dx.doi.org/10.1038/s41598-023-40281-8

Ejemplares similares