Three-dimensional optimization of squealer-tip for a transonic axial-flow compressor rotor blade
This research represents an innovative method for geometry generation of the squealer-tip in axial compressor rotors and its exploit in a numerical optimization process to obtain a better stage performance. For this purpose, the NASA Rotor-67 transonic compressor rotor blade is used as a test case t...
Tallennettuna:
| Päätekijät: | , , |
|---|---|
| Aineistotyyppi: | Artigo |
| Kieli: | Inglês |
| Julkaistu: |
Elsevier
2024-01-01
|
| Sarja: | Heliyon |
| Aiheet: | |
| Linkit: | http://www.sciencedirect.com/science/article/pii/S2405844023108735 |
| Tagit: |
Ei tageja, Lisää ensimmäinen tagi!
|