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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...
| Autores principales: | , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
Nature Publishing Group UK
2022
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| Materias: | |
| 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 |