Abstract
Russia's OPTIKA numerical optimization program is used for calculating the characteristic of a four-stage axial flow compressor's aerodynamic design. The performance of compressor is calculated and analyzed at collected speed n̄ = 1.0, 0.9. In the aerodynamic design process, the performances at the design and off-design points are considered simultaneously. The off-design aerodynamic characteristic optimization is expected to enhance the integrated performance of multistage axial flow compressor.
| Original language | English |
|---|---|
| Pages (from-to) | 583-585 |
| Number of pages | 3 |
| Journal | Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics |
| Volume | 28 |
| Issue number | 4 |
| State | Published - Jul 2007 |
Keywords
- Axial flow compressor
- Gas turbine
- Numerical simulation
- Optimization
- Turbomachinery
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