Numerical study of lateral coolant jet on heat reduction over nose cone with double-aerodome at hypersonic flow

One of the main challenges in designing a supersonic forebody is thermal protection. The application of the mechanical spike mounted at the nose considerably decreases the heat load on the main body. In this investigation, the hybrid technique of mechanical spike and coolant injection are examined t...

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Detalles Bibliográficos
Autores principales: Ghanbari, Mehdi, Maddah, Soroush, Alinejad, Javad
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Nature Publishing Group UK 2022
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9701809/
https://www.ncbi.nlm.nih.gov/pubmed/36437263
http://dx.doi.org/10.1038/s41598-022-22061-y

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9701809/
https://www.ncbi.nlm.nih.gov/pubmed/36437263
http://dx.doi.org/10.1038/s41598-022-22061-y

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