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射流控制水翼空化流動(dòng)的多工況適應(yīng)性研究
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國(guó)家自然科學(xué)基金項(xiàng)目(51876022)和國(guó)家重點(diǎn)基礎(chǔ)研究發(fā)展計(jì)劃項(xiàng)目(2015CB057301)


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

    空化時(shí)常會(huì)使船舶推進(jìn)器,、泵,、水輪機(jī)等水力機(jī)械部件產(chǎn)生噪聲、振動(dòng)和腐蝕,,導(dǎo)致設(shè)備總體性能的大幅下降,,甚至破壞,因此開展空化流動(dòng)控制具有重要意義,。借助高速全流場(chǎng)測(cè)試技術(shù),,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(duì)空化抑制的影響規(guī)律,,分析主動(dòng)射流在變工況下對(duì)空化流動(dòng)控制的適應(yīng)性,。研究發(fā)現(xiàn):在不同工況下,,主動(dòng)射流均可以取得明顯的空化抑制效果,當(dāng)射流流量及射流位置不同時(shí),,空化流動(dòng)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(zhǎng)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(zhǎng)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(shí)現(xiàn)對(duì)空化流場(chǎng)的主動(dòng)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(shí),,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(shí)驗(yàn)獲得最佳空化抑制有效性參數(shù)的偏差均在0.06以內(nèi),,H1模型表現(xiàn)出良好的工況適應(yīng)性,可實(shí)現(xiàn)多工況下空化的流動(dòng)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(dòng)的多工況適應(yīng)性研究[J].農(nóng)業(yè)機(jī)械學(xué)報(bào),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
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