Experimental and Numerical Investigation of a Novel Vortex Reducer in a Co-Rotating Cavity of Aeroengines
Improving airflow pressure is of great significance for the cooling and sealing of aeroengines. In a co-rotating cavity with radial inflow, vortex reducers are used to decrease the pressure drop. However, the performance of traditional vortex reducers is limited by their drag reduction mechanism and...
| Auteurs principaux: | , , , , |
|---|---|
| Format: | Article |
| Langue: | English |
| Publié: |
MDPI AG
2024-03-01
|
| Collection: | Aerospace |
| Sujets: | |
| Accès en ligne: | https://www.mdpi.com/2226-4310/11/3/225 |