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Combined effects of Reynolds number, turbulence intensity and periodic unsteady wake flow conditions on boundary layer development and heat transfer of a low pressure turbine blade

机译:雷诺数,湍流强度和周期性非稳态尾流条件对低压涡轮叶片边界层发展和传热的综合影响

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摘要

Detailed experimental investigation has been conducted to provide a detailed insightinto the heat transfer and aerodynamic behavior of a separation zone that is generated as aresult of boundary layer development along the suction surface of a highly loaded lowpressure turbine (LPT) blade. The research experimentally investigates the individual andcombined effects of periodic unsteady wake flows and freestream turbulence intensity (Tu)on heat transfer and aerodynamic behavior of the separation zone. Heat transfer experimentswere carried out at Reynolds number of 110,000, 150,000, and 250,00 based on the suctionsurface length and the cascade exit velocity. Aerodynamic experiments were performed atRe = 110,000 and 150,000. For the above Re-numbers, the experimental matrix includesTus of 1.9%, 3.0%, 8.0%,13.0% and three different unsteady wake frequencies with thesteady inlet flow as the reference configuration. Detailed heat transfer and boundary layermeasurements are performed with particular attention paid to the heat transfer andaerodynamic behavior of the separation zone at different Tus at steady and periodicunsteady flow conditions. The objectives of the research are (a) to quantify the effect of Tuon the aero-thermal behavior of the separation bubble at steady inlet flow condition, (b) toinvestigate the combined effects of Tu and the unsteady wake flow on the aero-thermalbehavior of the separation bubble, and (c) to provide a complete set of heat transfer andaerodynamic data for numerical simulation that incorporates Navier-Stokes and energyequations. The analysis of the experimental data reveals details of boundary layer separationdynamics which is essential for understanding the physics of the separation phenomenonunder periodic unsteady wake flow and different Reynolds number and Tu. To provide acomplete picture of the transition process and separation dynamics, extensive intermittencyanalysis was conducted. Ensemble averaged maximum and minimum intermittencyfunctions were determined leading to the relative intermittency function. In addition, thedetailed intermittency analysis reveals that the relative intermittency factor follows aGaussian distribution confirming the universal character of the relative intermittencyfunction.
机译:已经进行了详细的实验研究以提供对分离区的热传递和空气动力学行为的详细了解,该分离区是由于沿高负荷低压涡轮机(LPT)叶片的吸力面边界层发展而产生的。该研究通过实验研究了周期性非恒定尾流和自由流湍流强度(Tu)对分离区的传热和空气动力学行为的单独影响。基于吸力表面长度和级联出口速度,在雷诺数分别为110,000、150,000和250,00时进行了传热实验。在Re = 110,000和150,000时进行了空气动力学实验。对于以上Re-numbers,实验矩阵包括1.9%,3.0%,8.0%,13.0%的Tus和三个不同的非稳态唤醒频率,以稳定的入口流量作为参考配置。进行详细的传热和边界层测量时,要特别注意分离区在稳态和周期性非稳态流动条件下不同Tus的传热和空气动力学行为。研究的目的是(a)量化Tuon在稳定入口流量条件下分离气泡的空气热行为的影响,(b)研究Tu和非恒定尾流对空气的热行为的综合影响。 (c)为包含Navier-Stokes和能量方程的数值模拟提供完整的传热和空气动力学数据集。对实验数据的分析揭示了边界层分离动力学的细节,这对于理解周期性非恒定尾流和不同雷诺数和Tu下分离现象的物理性质至关重要。为了提供过渡过程和分离动力学的完整图片,进行了广泛的间歇分析。确定集合平均的最大和最小间断函数,从而得到相对间断函数。此外,详细的间歇性分析表明,相对间歇性因子遵循高斯分布,从而证实了相对间歇性函数的通用性。

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    Ozturk Burak;

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  • 年度 2009
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  • 原文格式 PDF
  • 正文语种 en_US
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