Full Annulus Simulations of a Transonic Axial Compressor Stage with Distorted Inflow at Transonic and Subsonic Blade Tip Speed
This article reports on systematic numerical studies on an axial compressor stage with distorted inflow. Four operating points at two speedlines were simulated with an inflow distortion generated by a 120 ∘ -sector segment with a wedge-type cross-section. With this setup, the interaction betw...
Gorde:
| Egile Nagusiak: | , |
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| Formatua: | Artigo |
| Hizkuntza: | Inglês |
| Argitaratua: |
MDPI AG
2018-02-01
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| Saila: | International Journal of Turbomachinery, Propulsion and Power |
| Gaiak: | |
| Sarrera elektronikoa: | http://www.mdpi.com/2504-186X/3/1/7 |
| Etiketak: |
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