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射流控制水翼空化流動的多工況適應性研究
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國家自然科學基金項目(51876022)和國家重點基礎研究發(fā)展計劃項目(2015CB057301)


Adaptability of Cavitation Flow Controlled by Active Jet under Multi-cavitation Conditions
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    摘要:

    空化時常會使船舶推進器、泵、水輪機等水力機械部件產生噪聲、振動和腐蝕,導致設備總體性能的大幅下降,甚至破壞,因此開展空化流動控制具有重要意義。借助高速全流場測試技術,獲得NACA66(MOD)原始水翼及射流水翼表面的空化形態(tài),研究射流控制參數(shù)對空化抑制的影響規(guī)律,分析主動射流在變工況下對空化流動控制的適應性。研究發(fā)現(xiàn):在不同工況下,主動射流均可以取得明顯的空化抑制效果,當射流流量及射流位置不同時,空化流動控制效果不同。在云空化階段,射流水孔與水翼前緣距離與弦長比值為0.19(H1模型)可以收到較好的空化抑制效果,且始終優(yōu)于H2模型;而在片空化階段,射流水孔與水翼前緣距離與弦長比值為0.45(H2模型)空化抑制效果更優(yōu)。不同的射流流量系數(shù)可以實現(xiàn)對空化流場的主動控制,且存在最佳射流流量系數(shù),使空化抑制效果最優(yōu)。在給定射流位置(H1模型)和射流流量(流量系數(shù)為0.0245)時,在空化不斷發(fā)展過程中(0.83≤σ≤1.46),空化抑制效果較為穩(wěn)定,與實驗獲得最佳空化抑制有效性參數(shù)的偏差均在0.06以內,H1模型表現(xiàn)出良好的工況適應性,可實現(xiàn)多工況下空化的流動控制。

    Abstract:

    Cavitation often causes noise, vibration and corrosion of hydraulic mechanical components such as ship propellers, pumps, and turbines, and causes the overall performance of the equipment to be greatly reduced, or even destroyed. Therefore, it is of great significance to carry out cavitation flow control. The method of arranging injection water holes on the suction side of the hydrofoil can effectively block the reentrant jet to suppress cavitation. Through the highspeed visual flow field test technology, the cavitation morphology of NACA66 (MOD) original hydrofoil and jet hydrofoil surfaces was obtained. The influence of jet control parameters on cavitation suppression was studied, and the adaptability of active jet to cavitation flow control under varying operating conditions was analyzed. It was found that under different cavitation conditions, the active jet significantly reduced the cavity length around the suction surface of the hydrofoil, and the cavitation suppression effect was significant. When the jet coefficient and jet position were different, the effect of cavitation flow control was also different. In the cloud cavitation stage, the jet of 0.19 chordlength position from the leading edge of the hydrofoil (H1 model) can achieve the best cavitation suppression effect, and it was always better than that of the H2 model in the range of cavitation number σ≤1.28. In the sheet cavitation stage, σ>1.44, the jet of 0.45 chordlength position from the leading edge of the hydrofoil (H2 model) was more effective in suppressing cavitation. When the fixed jet position (H1 model) and jet flow rate (flow coefficient was 0.0245), simplified flow control process, during the continuous development of cavitation (cavitation number was with 0.83≤σ≤1.46), the cavitation suppression effect was relatively stable, the deviation from the best suppression effect was within 0.06, which showed that the H1 model had good adaptability to working conditions. The research results provided a direction for exploring the active control technology of cavitation flow.

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王巍,安昭陽,唐滔,張慶典,王曉放.射流控制水翼空化流動的多工況適應性研究[J].農業(yè)機械學報,2020,51(10):186-194. WANG Wei, AN Zhaoyang, TANG Tao, ZHANG Qingdian, WANG Xiaofang. Adaptability of Cavitation Flow Controlled by Active Jet under Multi-cavitation Conditions[J]. Transactions of the Chinese Society for Agricultural Machinery,2020,51(10):186-194.

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  • 收稿日期:2019-12-16
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  • 在線發(fā)布日期: 2020-10-10
  • 出版日期: 2020-10-10