Numerical investigation on film cooling effectiveness of stator blade with or without heat transfer
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Numerical investigation on film cooling effectiveness of stator blade with or without heat transfer
Vol. 23, Issue 9, (2008)
作者机构:
1. 南京航空航天大学能源与动力学院,南京,210016
2. 中国燃气涡轮研究院,成都,610500
作者简介:
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DOI:
CLC:
Published:2008
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YAO Yu, ZHANG Jing-zhou, GUO Wen. Numerical investigation on film cooling effectiveness of stator blade with or without heat transfer[J]. 2008, 23(9).
DOI:
YAO Yu, ZHANG Jing-zhou, GUO Wen. Numerical investigation on film cooling effectiveness of stator blade with or without heat transfer[J]. 2008, 23(9).DOI:
Numerical investigation on film cooling effectiveness of stator blade with or without heat transfer
The film cooling effectiveness on the blade surface under different coolant entrance pressures was numerically investigated using the shear-stress transport(SST) two-equation turbulent model
so as to understand the influences of film-cooling holes on cooling effectiveness.Three-dimensional turbulent flow in the turbine cascade and the cooling effectiveness on the blade surface with cylindrical film cooling hole were simulated in two cases: with/without heat transfer in the blade.The results show that the cooling effectiveness increases with the increment of the coolant entrance total pressure
and the cooling effectiveness with heat transfer in the blade is better than that without heat transfer in the blade