Numerical Study on the Corner Separation Control for a Compressor Cascade via Bionic Herringbone Riblets
Bionic herringbone riblets are applied to relieve the flow near the blade endwall in a linear compressor cascade under the incidence angle of −4° to 6° at a Reynolds number of 382,000. The herringbone riblets are placed at the endwall upstream of the blade, and the Reynolds-averaged Navier–Stokes si...
Gorde:
| Egile Nagusiak: | , , |
|---|---|
| Formatua: | Artigo |
| Hizkuntza: | Inglês |
| Argitaratua: |
MDPI AG
2024-01-01
|
| Saila: | Aerospace |
| Gaiak: | |
| Sarrera elektronikoa: | https://www.mdpi.com/2226-4310/11/1/90 |
| Etiketak: |
Etiketarik gabe, Izan zaitez lehena erregistro honi etiketa jartzen!
|