Effect of rotor speed on heat transfer of blades:numerical simulation
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Effect of rotor speed on heat transfer of blades:numerical simulation
Thermal Power GenerationVol. 44, Issue 7, Pages: 23-27(2015)
作者机构:
东北电力大学能源与动力工程学院
作者简介:
基金信息:
DOI:
CLC:TK471
Published:2015
稿件说明:
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ZHANG Ling, WANG Chong. Effect of rotor speed on heat transfer of blades:numerical simulation[J]. Thermal power generation, 2015, 44(7): 23-27.
DOI:
ZHANG Ling, WANG Chong. Effect of rotor speed on heat transfer of blades:numerical simulation[J]. Thermal power generation, 2015, 44(7): 23-27.DOI:
Effect of rotor speed on heat transfer of blades:numerical simulation
摘要
为了研究尾迹脱落频率对动叶传热及其气膜冷却效率的影响
采用SSTk-ω紊流模型
在Simple算法基础上
利用有限体积法对无气膜孔和前缘有3排气膜孔情况下
转速分别为500
1 000
2 000r/min时动叶表面的努赛尔数(Nu)分布进行数值模拟。结果表明:随着转速的增大
无孔和有孔时的冷却效果差异明显
无孔时随转速增加动叶压力面和吸力面Nu逐渐降低
传热效果较差
有孔时则相反
换热增强
冷却效果较好。
Abstract
To investigate the effect of vertex shedding frequency on heat transfer and gas film cooling of the rotor blade
on the basis of Simple algorithm
the SSTk-ωturbulence model and finite volume method were adopted to discrete the control equations.Under conditions with no film-cooling hole and three rows of film-cooling holes at front edge of the blade
the effect of rotor speed on gas film cooling performance was numerically studied.The rotor speeds of 500r/min
1 000r/min and 2 000r/min were selected as the simulation conditions.The Nusselt number distribution on rotor surface was obtained.The results show that
with the increasing rotor speed
there's dramatic difference in cooling effectness between the blade with no film-cooling hole and the one with three rows of film-cooling holes.For the rotor with no film-cooling hole
the Nusselt number on pressure side and suction side of the rotor reduced gradually with an increase in rotor speed
so the heat transfer performance was relatively poor.While for the rotor with three rows of filmcooling holes
the heat transfer was enhanced and the film cooling efficiency was higher.
Numerical simulation of influence of equivalence ratio on combustion and NOx formation in a DLE combustor
Influence of coolant crossflow on film cooling effectiveness of one-inlet and double-outlet injection holes
Effects of unsteady wake on heat transfer performance of compound angle blade:numerical simulation
Effects of attack angle and endwall slippage on flow and heat transfer of blade squealer tip
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Related Institution
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