摘要
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.
源语言 | 英语 |
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页(从-至) | 13-17 |
页数 | 5 |
期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
卷 | 24 |
期 | 1 |
出版状态 | 已出版 - 1月 2009 |