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Large-Eddy Simulation and Passive Control of Flows for a Low Pressure Turbine Cascade

机译:低压涡轮叶栅流动的大涡模拟和被动控制

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A rectangular bar which just likes a forward-backward facing step was designed to passive control of the Low-Pressure Turbine (LPT) PakB cascade suction surface separation. Large-eddy simulation (LES) was adopted to analyze the separated-transition flows for the PakB cascade with and without the rectangular bar at Re (Reynolds number based on inlet condition and axial chord) of 86,000 and the freestream turbulence intensity of 1%. Computed results of uncontrolled condition agree well with the experimental data of Lake et al.[6, 7]. And the LES results shown that the rectangular bar control device was successful to control the LPT cascade suction surface separation and provides about 10% kinetic loss coefficient reduction from the uncontrolled one. Unsteady flow structures were also investigated in detail. Static pressure fluctuation frequency at six locations, ranging from 0.56C_xto 0.95C_x axial chord location and with a constant wallnormal distance y/h=1.0, was the same to the separation bubble vortex shedding frequency. Unsteady fluctuation velocity was examined too, which confirmed that the separation bubble vortex frequency was the same to the suction surface static pressure fluctuation frequency.
机译:设计了一个矩形矩形条,它像向前和向后的台阶一样,用于被动控制低压涡轮(LPT)PakB级联吸入表面的分离。采用大涡模拟(LES)来分析带有和不带有Re(基于入口条件和轴向弦的雷诺数)的矩形棒的PakB级联的分离过渡流,该分离流为86,000,自由流湍流强度为1%。不受控制条件的计算结果与Lake等人的实验数据非常吻合[6,7]。 LES结果表明,矩形棒控制装置成功地控制了LPT级联吸力表面的分离,与未控制的装置相比,其动损耗系数降低了约10%。还对非定常流动结构进行了详细研究。六个位置的静压波动频率,范围从0.56C_x 至0.95C_x轴向弦位置并具有恒定的壁 正常距离y / h = 1.0,与分离气泡涡旋脱落频率相同。还检查了不稳定波动速度,这证实了分离气泡涡旋频率与吸力表面静压力波动频率相同。

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