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Improved aerodynamic design of turbomachinery bladings by numerical optimization
| Content Provider | Semantic Scholar |
|---|---|
| Author | Burguburu, Stéphane Pape, Arnaud Le |
| Copyright Year | 2003 |
| Abstract | Abstract The aerodynamic optimization of a transonic compressor is reported in this paper. The Q3D Navier–Stokes solver COLIBRI is coupled to a gradient-based method (CONMIN) and to a genetic algorithm (GADO). The suction side of a 2D blade is optimized by using both optimization methods with a significant efficiency improvement. In 3D, the performance improvement is obtained by modifying the suction surface of a transonic compressor with a Bezier surface and by using the CANARI solver coupled to the gradient method (CONMIN). |
| Starting Page | 277 |
| Ending Page | 287 |
| Page Count | 11 |
| File Format | PDF HTM / HTML |
| DOI | 10.1016/S1270-9638(02)00010-X |
| Alternate Webpage(s) | http://isiarticles.com/bundles/Article/pre/pdf/10416.pdf |
| Alternate Webpage(s) | https://doi.org/10.1016/S1270-9638%2802%2900010-X |
| Volume Number | 7 |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |
