Abstract
In this paper, based on the Modified Nested Sparse-grid Stochastic Collocation (MNSSC) method, the influence of the random error of the turbine blade stagger angle on the aerodynamic performance of the cascade is studied. The results show that the MNSSC method overcomes the curse of dimension, reduces the number of high-dimensional samples and avoids the waste of samples. The MNSSC method can quickly and effectively simulate the propagation of multiple uncertainties in the internal flow field; The influence of uncertainties on the suction side is significantly greater than that on the pressure side, and it has the greatest influence on the suction side of 40%Cax; the uncertainties of the stagger angle affect the flow field along the A direction, and its mainly affects areas with large velocity gradients such as separation regions.
| Translated title of the contribution | Uncertainty Quantification in Blade Stagger Angle Based on MNSSC Method |
|---|---|
| Original language | Chinese (Traditional) |
| Pages (from-to) | 2705-2712 |
| Number of pages | 8 |
| Journal | Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics |
| Volume | 44 |
| Issue number | 10 |
| State | Published - Oct 2023 |
| Externally published | Yes |
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