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A Detailed Uncertainty Analysis of Adiabatic Film Cooling Effectiveness Measurements Using Pressure-Sensitive Paint

机译:使用压敏涂料的绝热膜冷却效果测量的详细不确定度分析

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摘要

Pressure-sensitive paint (PSP) can be a powerful tool in measuring the adiabatic film cooling effectiveness. There are two distinct sources of error for this measurement technique: the ability to experimentally obtain the data and the validity of the heat and mass transfer analogy for the problem being studied. This paper will assess the experimental aspect of this PSP measurement specifically for film cooling applications. Experiments are conducted in an effort to quantifiably bound expected errors associated with temperature nonuniformities in testing and photodegradation effects. Results show that if careful experimental procedures are put in place, both of these effects can be maintained to have less than 0.022 impact on effectiveness. Through accurate semi in situ calibration down to 4% atmospheric pressure, the near-hole distribution of effectiveness is measured with high accuracy. PSP calibrations are performed for multiple coupons, over multiple days. In addition, to reach a partial pressure of zero the calibration vessel was purged of all air by flowing CO_2. The primary contribution of this paper lies in the uncertainty analysis performed on the PSP measurement technique. A thorough uncertainty analysis is conducted and described, in order to completely understand the presented measurements and any shortcomings of the PSP technique. This quantification results in larger, albeit more realistic, values of uncertainty and helps provide a better understanding of film cooling effectiveness measurements taken using the PSP technique. The presented uncertainty analysis takes into account all random error sources associated with sampling and calibration, from intensities to effectiveness. Adiabatic film cooling effectiveness measurements are obtained for a single row of film cooling holes inclined at 20 deg, with CO_2 used as coolant. Data are obtained for six blowing ratios. Maps of uncertainty corresponding to each effectiveness profile are available for each test case. These maps show that the uncertainty varies spatially over the test surface and high effectiveness corresponds to low uncertainty. The noise floors can be as high as 0.04 at effectiveness levels of 0. Day-to-day repeatability is presented for each blowing ratio and shows that laterally averaged effectiveness data are repeatable within 0.02 effectiveness.
机译:压敏涂料(PSP)是衡量绝热膜冷却效果的有力工具。此测量技术有两个不同的误差源:通过实验获得数据的能力以及对所研究问题进行传热和传质模拟的有效性。本文将评估此PSP测量的实验方面,专门针对薄膜冷却应用。进行实验是为了量化地限制与测试和光降解效应中温度不均匀性相关的预期误差。结果表明,如果采取了周密的实验程序,则可以保持这两种效果对有效性的影响小于0.022。通过精确的半原位校准(低至4%大气压),可以高精度测量近孔有效性分布。 PSP校准会在多天内针对多个优惠券执行。另外,为了达到零分压,通过流动CO_2清除校准容器中的所有空气。本文的主要贡献在于对PSP测量技术进行的不确定性分析。进行并进行了彻底的不确定性分析,以完全理解所提出的测量结果和PSP技术的任何缺点。这种量化可以带来更大,更现实的不确定性值,并有助于更好地理解使用PSP技术进行的薄膜冷却效果测量。提出的不确定性分析考虑了与采样和校准相关的所有随机误差源,从强度到有效性。对于倾斜20度的单排薄膜冷却孔,使用CO_2作为冷却剂,获得了绝热薄膜冷却效率的测量结果。获得了六个吹风比的数据。每个测试案例都可以使用与每个有效性概况相对应的不确定性图。这些图表明,不确定性在测试表面上在空间上变化,并且高有效性对应于低不确定性。在0的有效水平下,本底噪声可以高达0.04。每个吹风比的日常重复性均得到显示,并显示横向平均有效性数据在0.02的有效性内可重复。

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  • 来源
    《Journal of turbomachinery》 |2016年第8期|081007.1-081007.12|共12页
  • 作者单位

    Department of Mechanical and Aerospace Engineering, University of Central Florida, Orlando, FL 32816;

    Department of Mechanical and Aerospace Engineering, University of Central Florida, Orlando, FL 32816;

    Department of Mechanical and Aerospace Engineering, University of Central Florida, Orlando, FL 32816;

    GE Global Research, Niskayuna, NY 12309;

    GE Aviation, Lynn, MA 01905;

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