Abstract
The numerical simulation of influences of unsteady wake on the time-average heat transfer of turbine blade was made by introducing the concept of wake induced transitional time-averaged intermittency and putting forward methods for calculating both normal transition onset and wake induced transition onset. The agreement between predictions and experimental data is good both on suction surface and pressure surface of turbine blade.
| Original language | English |
|---|---|
| Pages (from-to) | 53-56 |
| Number of pages | 4 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 20 |
| Issue number | 4 |
| State | Published - 1999 |
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