Experimental study of the discharge coefficient of film outflow varying with the internal cooling channel’s height
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Experimental study of the discharge coefficient of film outflow varying with the internal cooling channel’s height
Vol. 26, Issue 3, (2011)
作者机构:
1. 南京航空航天大学 能源与动力学院,南京,210016
2. 上海飞机设计研究院 动力燃油设计研究部,上海,200232
3. 中国航空工业集团公司 中国燃气涡轮研究院 涡轮室,成都,610500
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Published:2011
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MAO Jun-kui, HU Bo, SU Yun-liang, et al. Experimental study of the discharge coefficient of film outflow varying with the internal cooling channel’s height[J]. 2011, 26(3).
DOI:
MAO Jun-kui, HU Bo, SU Yun-liang, et al. Experimental study of the discharge coefficient of film outflow varying with the internal cooling channel’s height[J]. 2011, 26(3).DOI:
Experimental study of the discharge coefficient of film outflow varying with the internal cooling channel’s height
According to the heat transfer enhancement with vortex
experiments were performed to investigate the discharge coefficient of film outflow in narrow confined space
which the ratio of the internal cooling channel height to the diameter of film cooling hole (h/d) was smaller than 1.In experiments
the rules of discharge coefficient Cd varying with the film cooling hole Reynolds number (4800~26000)
blowing rate M(0.36~2.74)
dimensionless of film cooling channel height h/d(0.33~2.0)were studied in detail
and the similarity criteria for discharge coefficients varying with these parameters were concluded.The experimental results show that the film cooling hole discharge coefficient increase with the film cooling hole Reynolds number when the main flow Reynolds number is constant.In the constant film cooling hole Reynolds number cases
Cd increase with the blowing rate M rising especially when M is smaller than 1.It is also found in experiments that the Cd decrease with dimensionless of film cooling channel height h/d increasing
especially in the cases which the film cooling hole Reynolds number is larger than 9500.