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Numerical study of hydrofoil surface jet flow on cavitation suppression 被引量:6
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作者 WANG Wei LU Shengpeng +3 位作者 XU Ruiduo YI Qi WANG Yayun WANG Xiaofang 《排灌机械工程学报》 EI CSCD 北大核心 2017年第10期829-834,共6页
Cavitation caused vibration and noise of hydraulic machinery. To some extent,cavitation made fatigue damage in advance. Many scholars found that the re-entrant jets were the reasons of the shedding of cavities. To sup... Cavitation caused vibration and noise of hydraulic machinery. To some extent,cavitation made fatigue damage in advance. Many scholars found that the re-entrant jets were the reasons of the shedding of cavities. To suppress cavitation,based on the idea of blocking the re-entrant jets,a special surface flow structure of 2D hydrofoil was proposed. The through-hole was made in the proper position of the hydrofoil. The incoming flow can outflow from this jet-hole automatically depending on the pressure difference between pressure side and suction side. Re-entrant jet growth can be weakened by optimizing the jet-hole geometry. Based on the standard k-ε turbulence model and Schnerr & Sauer cavitation model,under different cavitation numbers( σ) and jet-angles( β) for NACA0066( 2D) hydrofoil with 8° angles of attack,cavitation field numerical analysis was carried out. The results show that 2D hydrofoil cavitation flow had a strong unsteadiness. Making a jet-hole at the junction between the re-entrant jet and cavity can effectively minimize cloud cavitation. For a certain cavitation condition,optimal jet-angles( β) can be obtained to control cavitation growth. For the same β,the effects of cavitation suppression were changed with different cavitation numbers( σ). Consequently,suitable jet-angle and jet-position could extend the stable operating range of the hydrofoil. 展开更多
关键词 hydrofoil cavitation suppression jet flow lift-to-drag ratio
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Adaptability research of hydrofoil surface water injection on cavitation suppression 被引量:4
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作者 WANG Wei YI Qi +2 位作者 WANG Yayun LU Shengpeng WANG Xiaofang 《排灌机械工程学报》 EI CSCD 北大核心 2017年第6期461-466,480,共7页
To study the effectiveness of hydrofoil surface water injection on cavitation suppression,the unsteady cavitation flow field around the NACA0066 hydrofoil at attack angle of 6°was simulated by the modified RNG k-... To study the effectiveness of hydrofoil surface water injection on cavitation suppression,the unsteady cavitation flow field around the NACA0066 hydrofoil at attack angle of 6°was simulated by the modified RNG k-εturbulence model combined with the full-cavitation model.The structure of cavitation flow field and the hydrodynamic performance of hydrofoil were analyzed at the cavitation number of 0.85,0.70,0.55,respectively.The results show that barriered by the jet,the momentum of the reentrant jet was reduced;The development of cavitation and the strength of cavity shedding were weakened to some extent.Cavitation suppression effect was very obvious in the cavitation conditions with the cavitation number of 0.7 and above when the injection position was at 37% chord length from the hydrofoil leading edge and the jet-flow ratio kept 0.3.Time-averaged lift and drag coefficient were reduced,and the lift-drag ratio increased in water injection conditions. 展开更多
关键词 hydrofoil cavitation suppression reentrant jet water injection jet-flow ratio
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水翼表面布置射流水孔抑制空化 被引量:9
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作者 王巍 羿琦 +2 位作者 林茵 徐瑞铎 王晓放 《排灌机械工程学报》 EI CSCD 北大核心 2016年第10期872-877,共6页
为研究水翼表面布置射流水孔对空化的抑制效果,采用RNG k-ε湍流模型结合全空化模型对8°攻角NACA0066(MOD)水翼进行二维非定常空化流场计算,分析当射流比分别为0.1,0.2和0.3时的水翼表面空化流场结构及其演化过程的流动特性,得到... 为研究水翼表面布置射流水孔对空化的抑制效果,采用RNG k-ε湍流模型结合全空化模型对8°攻角NACA0066(MOD)水翼进行二维非定常空化流场计算,分析当射流比分别为0.1,0.2和0.3时的水翼表面空化流场结构及其演化过程的流动特性,得到了不同射流条件下水翼升阻力系数的变化趋势.计算结果表明:布置射流水孔可以有效阻挡回射流从翼型尾部向翼型头部的运动,使得空泡脱落现象明显减弱,从而抑制了片空化向云空化的发展,且随射流比增加,射流对回射流和云空化的抑制作用更加显著;射流的注入同时使得升力系数和阻力系数的波动幅度明显降低,有效减弱了升阻力的周期性振荡;虽然时均升力和时均阻力受射流的影响有下降趋势,但升阻比呈上升趋势,水翼升阻比由无射流孔时的6.11增加到射流比为0.3时的7.06,布置射流孔还起到了减阻的作用. 展开更多
关键词 水翼 射流比 云空化 空化抑制 升阻比
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