Numerical investigation of compressible flow around nose cone with Multi-row disk and multi coolant jets

Due to sever aerodynamic heating, the protection of forebody of scramjet is crucial for hypersonic flight. In present work, a new cooling system is proposed and investigated for the protection of nose cone at hypersonic flight. Computational fluid dynamic is used for the simulation of the lateral an...

Descripción completa

Detalles Bibliográficos
Autores principales: Iranmanesh, Reza, Alizadeh, As’ad, Faraji, M., Choubey, Gautam
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/PMC9842636/
https://www.ncbi.nlm.nih.gov/pubmed/36646787
http://dx.doi.org/10.1038/s41598-023-28127-9

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9842636/
https://www.ncbi.nlm.nih.gov/pubmed/36646787
http://dx.doi.org/10.1038/s41598-023-28127-9

Ejemplares similares