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基于超大渦模擬的翼端間隙流湍流特性與損失機(jī)理分析
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Very Large Eddy Simulation Analysis of Turbulent Flow Characteristic and Mechanisms for Turbulent Loss in Hydrofoil Tip Clearance Flows
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    摘要:

    為探明不同翼端間隙條件下水翼端部間隙區(qū)湍流特征及間隙湍流損失機(jī)理,,以NACA0009型鈍尾緣水翼為研究對象,采用基于SST k-ω湍流模型的超大渦模擬方法,,分析了間隙寬度τ(分別為0.1c和0.02c)和翼端倒圓半徑r(分別為0,,0.5%c和1%c)對間隙區(qū)渦系結(jié)構(gòu),、湍流雷諾應(yīng)力、湍動能和湍流損失的影響,。結(jié)果表明,,不同間隙條件下,間隙流動的雷諾應(yīng)力分布與間隙渦系分布趨于一致,,以法向正應(yīng)力〈v′v′〉和展向正應(yīng)力〈w′w′〉為主,。大間隙下(τ=0.1c),湍動能和雷諾應(yīng)力主要分布在間隙分離渦區(qū)域,,速度梯度〈v〉/z和雷諾應(yīng)力〈w′w′〉主導(dǎo)間隙分離渦區(qū)域的湍動能生成,,隨翼端倒圓半徑增加,間隙湍流損失因間隙區(qū)雷諾應(yīng)力的顯著減小而降低,;小間隙下(τ=0.02c),,間隙端壁邊界層在間隙泄漏渦的強(qiáng)卷吸作用下形成誘導(dǎo)渦,間隙區(qū)湍流損失主要產(chǎn)生于間隙泄漏渦和誘導(dǎo)渦區(qū)域內(nèi),,隨翼端倒圓半徑增大而增大,,其原因是主導(dǎo)誘導(dǎo)渦湍動能生成的雷諾應(yīng)力〈v′v′〉與速度梯度〈v〉/y和主導(dǎo)間隙泄漏渦湍動能生成的〈v′w′〉與(〈v〉/z+〈w〉/y)均隨翼端倒圓半徑增加而增大。

    Abstract:

    The tip-leakage flows over an NACA0009 blunt trailing edge hydrofoil with different tip gap width (τ=0.1c and 0.02c, c is hydrofoil chord length) and tip edge rounding (rounding radius r=0, 0.5%c and 1%c) were studied by using SST k-ω turbulent model based very large eddy simulation (VLES) with particular emphasis on understanding the turbulence characteristics and the underlying mechanisms for turbulent loss in the vicinity of the tip gap. Systematic and detailed analysis of the vortex structures, Reynolds stresses, turbulent kinetic energy and tip clearance turbulent loss was made around the hydrofoil with a stationary endwall. Results showed that the Reynolds stress distributions in the tip gap region were consistent with the distributions of the tip clearance vortices, and the magnitude of the normal stresses 〈v′v′〉and 〈w′w′〉 around the tip gap vortices were larger than that of other Reynolds stress components. For the gap τ=0.1c, turbulent kinetic energy and Reynolds stresses of the tip clearance flow were found to be concentrated in the tip separated vortex (TSV) region, the velocity gradient 〈v〉/z and the spanwise normal stress 〈w′w′〉dominated the generation of turbulent kinetic energy in the TSV region; as the tip rounding radius increased, the significant decrease of the Reynolds stresses resulted in a reduction of the tip clearance turbulent loss. For gap size of 0.02c, the strong entrainment of the tip leakage vortex (TLV) on the end-wall boundary layer induced the formation of an induced vortex (IV), which rotated opposite to the TLV. The tip clearance turbulent loss mainly occurred in the TLV and IV regions for the smaller tip gap cases, and its magnitude was increased with the increase of the rounding radius. The underlying mechanism for this tendency was that enlarging the tip clearance increased the normal Reynolds stress 〈v′v′〉 and the velocity gradient 〈v〉/y, which dominated the production of turbulent kinetic energy in the IV region; and it also led to an increase of the Reynolds shear stress 〈v′w′〉 and velocity gradient 〈v〉/z+〈w〉/y), which dominated the generation of turbulent kinetic energy in the TLV region.

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陳為升,黎耀軍,劉竹青,楊魏.基于超大渦模擬的翼端間隙流湍流特性與損失機(jī)理分析[J].農(nóng)業(yè)機(jī)械學(xué)報,2022,53(8):144-153. CHEN Weisheng, LI Yaojun, LIU Zhuqing, YANG Wei. Very Large Eddy Simulation Analysis of Turbulent Flow Characteristic and Mechanisms for Turbulent Loss in Hydrofoil Tip Clearance Flows[J]. Transactions of the Chinese Society for Agricultural Machinery,2022,53(8):144-153.

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  • 收稿日期:2021-08-14
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  • 在線發(fā)布日期: 2021-09-14
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