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Throttling process of a supersonic cascade studied by high-frequency response pressure and high-speed schlieren
In this study, a single-channel supersonic cascade model is investigated experimentally at a freestream Mach number of 2.4 to obtain a better understanding of the flow field evolution during the throttling process. A flap is placed at the channel exit to choke the flow linearly. Measurements include...
| Autores principales: | , , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
| Publicado: |
Nature Publishing Group UK
2021
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| Materias: | |
| Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8245612/ https://www.ncbi.nlm.nih.gov/pubmed/34193916 http://dx.doi.org/10.1038/s41598-021-93021-1 |