Experimental investigation of heat transfer and pressure drop in a two-pass internal coolant passages of gas turbine airfoil
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Experimental investigation of heat transfer and pressure drop in a two-pass internal coolant passages of gas turbine airfoil
Vol. 25, Issue 12, (2010)
作者机构:
清华大学 机械工程学院 热能工程系 燃气轮机研究中心,北京,100084
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Published:2010
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CHEN Wei, KAN Rui, REN Jing, et al. Experimental investigation of heat transfer and pressure drop in a two-pass internal coolant passages of gas turbine airfoil[J]. 2010, 25(12).
DOI:
CHEN Wei, KAN Rui, REN Jing, et al. Experimental investigation of heat transfer and pressure drop in a two-pass internal coolant passages of gas turbine airfoil[J]. 2010, 25(12).DOI:
Experimental investigation of heat transfer and pressure drop in a two-pass internal coolant passages of gas turbine airfoil
An experimental investigation was conducted to assess the heat transfer and pressure drop distribution of a two-pass channel with a round turn.The Reynolds numbers investigated varied from 30000 to 55000.This demonstrates that the secondary flow induced by ribs is the main factor to enhance the heat transfer before turn region.Under different Reynolds numbers
the trend of heat transfer and pressure drop distribution in the duct is consistent.However
the heat transfer in the after turn region is different.Moreover
the largest pressure drop occurs in the turn region.As the Reynolds number increases
the loss coefficient of the turn and the whole duct will decrease.Compared with two-pass channel with a sharp turn
the heat transfer in the turn region and after turn region in this study is lower
because the acceleration effect in the round turn region is not as strong as that in sharp turn.