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发表时间：2022-10-06

发表刊物：航空动力学报

所属单位：能源与动力学院

期号：1

页面范围：71-76

ISSN号：1000-8055

摘要：3-D Navier-Stokes equations were solved with the conventional k-Ε turbulence model to predict turbulent flow and heat transfer in the internal cooling passage of the gas turbine blades, in which the staggered arrays of discrete helix-alike rectangular-fins or wedged-fins with a certain angle were used along two inside opposite walls. Results were presented for Reynolds number in the range of 1 × 104 to 2 × 105, cross-section aspect ratio of 2.9, fin height to hydraulic diameter ratio of 0.336, fin height to passage height ratio of 0.5, and the inclined angle of the helix-alike fin of 15°. A complicated 3-D accelerated spiral-flow which just likes the fluid flow in helical-fin tube has been formed and it has significant effects on the heat transfer. The averaged Nusselt number ratios decrease and the friction factor ratios increase with the increasing Reynolds number for all the studied cases. Also the detailed discussion of the influence of helix-alike fin surface shape on heat transfer and pressure drop was given. It is found that, the heat transfer enhancement in the internal cooling passage with helix-alike rectangular-fin is better than others, but the comprehensive enhancement performance ratio is lower than that with helix-alike fins.

备注：新增回溯数据