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Aerodynamic design by jointly applying S2 flow
surface calculation and modern optimization methods on multistage
axial turbine
- ZHAO Honglei, WANG Songtao, HAN Wanjin, FENG Guotai
Author information
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Academy of Energy Science and Engineering, Harbin Institute of Technology
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History
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| Published |
| 05 Mar 2008 |
| Issue Date |
| 05 Mar 2008 |
A three-stage axial turbine was redesigned by jointly applying S2 flow surface direct problem calculation methods and multistage local optimization methods. A genetic algorithm and artificial neural network were jointly adopted during optimization. A three-dimensional viscosity Navier–Stokes equation solver was applied for flow computation. H-O-H-topology grid was adopted as computation grid, that is, an H-topology grid was adopted for inlet and outlet segment, whereas an O-topology grid was adopted for stator zone and rotor zone. Through the optimization design, the total efficiency increases 1.1%, thus indicating that the total performance is improved and the design objective is achieved.
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References
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