Abstract
Numerical simulation was conducted to gain greater insight into the flow structure of trapezoidal pin-fin duct and get detailed knowledge of the heat transfer on the endwall surface. The array geometries have short pin heights and small chord-wise pin spacing. Numerical results show that, the calculated flow resistances and chord-wise ejection mass flow rate agree well with the experimental data, and the heat transfer pattern is well simulated. The numerical results also show that the flow direction in pin-fin region is mainly chord-wise. There are a lower velocity and lower turbulence intensity region behind the cylinder.
Original language | English |
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Pages (from-to) | 13-17 |
Number of pages | 5 |
Journal | Hangkong Dongli Xuebao/Journal of Aerospace Power |
Volume | 24 |
Issue number | 1 |
State | Published - Jan 2009 |
Keywords
- Cooling blade
- Flow and heat transfer
- Gas turbine
- Numerical simulation
- Small spacing pin-fin