不同去旋角度进气共转盘腔内流动与换热研究 |
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引用本文: | 杨守辉,王锁芳.不同去旋角度进气共转盘腔内流动与换热研究[J].航空发动机,2011,37(6):17-20. |
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作者姓名: | 杨守辉 王锁芳 |
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作者单位: | 南京航空航天大学能源与动力学院,南京,210016 |
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摘 要: | 以带有去旋喷嘴的共转盘腔为研究对象,运用RNG k-ε湍流模型,分别对3种喷嘴角度(90°、60°、30°)的3维模型进行了数值计算,揭示了去旋角度对盘腔内气体切向速度、盘腔内压降和转盘表面换热的影响规律。研究结果表明:随着去旋角度的减小,盘腔内气体的切向速度减小,盘腔内压降减小,转盘表面的局部努赛尔数Nur增大。
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关 键 词: | 共转盘腔 去旋角度 流动 数值计算 航空发动机 |
Investigation on Flow and Heat Transfer inside Co-rotating Disc Cavity
with Different De-swirl Angle |
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Authors: | YANG Shou-hui WANG Suo-fang |
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Institution: | (College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China) |
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Abstract: | The 3D numerical simulation of the co-rotating disc cavity with the de-swirl nozzles was carried by the RNG k-ε turbulence model with three kinds of de-swirl angles(90°,60°,and 30°).The influence of the de-swirl angle on the tangential velocity,the pressure loss in the disc cavity and the heat transfer of the rotational disc is discoverd.The results show that as the de-swirl angle reduces,the flow tangential velocity in the disc cavity decreases,the pressure loss in the disc cavity reduces,the local Nur number of the rotational disc surface increases. |
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Keywords: | co-rotating cavity de-swirl angle flow numerical calculation aeroengine |
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