Accurate 2-D Modelling of Transonic Compressor Cascade Aerodynamics
Modern aeronautic fans are characterised by a transonic flow regime near the blade tip. Transonic cascades enable higher pressure ratios by a complex system of shockwaves arising across the blade passage, which has to be correctly reproduced in order to predict the performance and the operative rang...
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| Autors principals: | , , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
MDPI AG
2019-05-01
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| Col·lecció: | Aerospace |
| Matèries: | |
| Accés en línia: | https://www.mdpi.com/2226-4310/6/5/57 |
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