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Study on film cooling flow characteristics of film holes in rounded corner crater
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Deheng ZHANG1, Yeguang HE1, 2, Tianhua YANG1, Tao ZHANG1, Tao DU2
Thermal Power Generation | 2024, 53(5) : 101 - 108
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Thermal Power Generation | 2024, 53(5): 101-108
Thermal energy science research
Study on film cooling flow characteristics of film holes in rounded corner crater
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Deheng ZHANG1, Yeguang HE1, 2, Tianhua YANG1, Tao ZHANG1, Tao DU2
Affiliations
  • 1.College of Energy and Environment, Shenyang Aerospace University, Shenyang 110136, China
  • 2.College of Metallurgy, Northeastern University, Shenyang 110819, China
Published: 2024-05-25 doi: 10.19666/j.rlfd.202401013
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In order to explore the film cooling potential of crater holes, numerical simulations are performed to investigate the film cooling characteristics of equal-section crater hole, concentric elliptical crater hole, and two types of rounded corner crater holes proposed on the basis of these two types of crater holes. Cooling efficiency curves are analyzed for four types of crater holes at blowing ratios of 0.5, 1.0 and 1.5. The results show that, the crater spreading width of crater holes and crater film holes with rounded corners increases, which is beneficial to spreading coverage of the cooling film. After the crater holes are rounded at three blowing ratios, the Coanda effect strengthenes the ability of the cooling jet to adhere to the wall, and the film cooling efficiency in the near-hole region improves significantly. As the blowing ratio increases, the area-averaged film cooling efficiency after the rounded corner treatment increases by 76%, 139% and 155%, respectively, for the equal-section crater hole. The area-averaged film cooling efficiency improves by 18%, 27%, and 29%, respectively, for the concentric-elliptical crater hole with rounded corner compared with that of the concentric-elliptical crater hole.

film cooling  /  turbine blade  /  rounded corner crater  /  numerical simulation  /  counter-rotating vortex pair
Deheng ZHANG, Yeguang HE, Tianhua YANG, Tao ZHANG, Tao DU. Study on film cooling flow characteristics of film holes in rounded corner crater[J]. Thermal Power Generation, 2024 , 53 (5) : 101 -108 . DOI: 10.19666/j.rlfd.202401013
  • Project of Liaoning Provincial Department of Education(JYT2020044)
Year 2024 volume 53 Issue 5
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101
42
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Article Info
doi: 10.19666/j.rlfd.202401013
  • Receive Date:2024-01-24
  • Online Date:2026-01-07
  • Published:2024-05-25
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  • Received:2024-01-24
Funding
Project of Liaoning Provincial Department of Education(JYT2020044)
Affiliations
    1.College of Energy and Environment, Shenyang Aerospace University, Shenyang 110136, China
    2.College of Metallurgy, Northeastern University, Shenyang 110819, China
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https://castjournals.cast.org.cn/joweb/rlfd/EN/10.19666/j.rlfd.202401013
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表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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