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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...
| Autores principales: | , , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
Nature Publishing Group UK
2023
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| Materias: | |
| 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 |