Abstract
A three-stage axial turbine was redesigned by using an aerodynamic optimization design process of multistage axial turbine in multiple working conditions, which combines quasi-3D design methods and multistage local optimization methods. Genetic algorithm and artificial neural network were employed to 3D local optimization of various cascades. The flow field was computed through a three-dimensional viscosity Navier-Stokes equation. With optimization design, the performance of every cascade was optimized, and the overall efficiency increased by 1% under the reliable total flow mass, indicating that the total performance was improved to satisfy the design requirements.
| Original language | English |
|---|---|
| Pages (from-to) | 106-111 |
| Number of pages | 6 |
| Journal | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| Volume | 23 |
| Issue number | 1 |
| State | Published - Jan 2008 |
| Externally published | Yes |
Keywords
- Aerospace propulsion system
- Artificial neural network
- Genetic algorithm
- Optimization design under multiple working conditions
- Turbine
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