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Framework of airfoil max lift-to-drag ratio prediction using hybrid feature mining and Gaussian process regression

机译:使用混合特征挖掘和高斯过程回归的翼型翼型最大升力比率预测

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摘要

The maximum lift-to-drag coefficient of an airfoil directly affects the aerodynamic performance of wind turbine. Machine learning methods are known for being really effective in helping to predict this parameter in a faster and more accurate way. So far, the majority of related studies have focused on the use of artificial neural networks to make this prediction, but this model has issues with its poor interpretation and the confidence level of its results was unclear. In this paper, a novel framework is proposed, involving the Gaussian process regression and a hybrid feature mining process. The aim is to use the new framework to evaluate the maximum lift-to-drag ratio of given airfoils under a turbulent flow condition, where the Reynolds number is around 100,000. The feature mining process here designed contains a hybrid feature pool that comprises various geometric characters, and a hybrid feature selector that can assist the prediction performance and make it better. Based on the airfoil dataset of the University of Illinois at Urbana-Champaign that contains a total of 1432 profiles, a comparative analysis was conducted. The results showed that the current framework can provide a more accurate estimate than parallel models in both single-point and interval aspects of view. Noticeably, the model reached an overall precision of 95.2% and 94.1% on training and testing sets, respectively. Moreover, the simplicity and the confidence reference from the model output were further illustrated with a case study, which also verified that how it can serve real engineering application.
机译:翼型的最大提升系数直接影响风力涡轮机的空气动力学性能。已知机器学习方法是为了帮助以更快更准确的方式预测该参数的真正有效。到目前为止,大多数相关研究都集中在利用人工神经网络来实现这一预测,但这种模式具有较差的解释和其结果的置信水平尚不清楚。本文提出了一种新颖的框架,涉及高斯过程回归和混合特征采矿过程。目的是使用新框架在湍流条件下评估给定翼型的最大提升比,其中雷诺数约为100,000。这里的特征挖掘过程设计包含一个混合特征池,包括各种几何字符,以及可以帮助预测性能并使其更好的混合特征选择器。基于伊利诺伊大学伊利诺伊州的亚洲杂船 - 康香委员会,其中包含总共1432个概况,进行了比较分析。结果表明,目前框架可以在单点和间隔方面,提供比并行模型更准确的估计。明显的是,该模型分别达到了95.2%的整体精度,培训和检测集分别为95.2%和94.1%。此外,通过案例研究进一步示出了模型输出的简单性和置信度,这也证实了它如何为实际工程应用程序提供服务。

著录项

  • 来源
    《Energy Conversion & Management》 |2021年第9期|114339.1-114339.14|共14页
  • 作者单位

    Shanghai Jiao Tong Univ Sch Naval Architecture Ocean & Civil Engn Shanghai 200240 Peoples R China;

    Shanghai Jiao Tong Univ Sch Naval Architecture Ocean & Civil Engn Shanghai 200240 Peoples R China;

    Shanghai Jiao Tong Univ Sch Naval Architecture Ocean & Civil Engn Shanghai 200240 Peoples R China;

    Shanghai Jiao Tong Univ Sch Naval Architecture Ocean & Civil Engn Shanghai 200240 Peoples R China;

    Shanghai Jiao Tong Univ Sch Naval Architecture Ocean & Civil Engn Shanghai 200240 Peoples R China|Shanghai Jiao Tong Univ State Key Lab Ocean Engn Shanghai 200240 Peoples R China|Shanghai Jiao Tong Univ Key Lab Hydrodynam Minist Educ Shanghai 200240 Peoples R China|Shanghai Jiao Tong Univ Shanghai Key Lab Digital Maintenance Bldg & Infra Shanghai 200240 Peoples R China;

    Shanghai Jiao Tong Univ Sch Naval Architecture Ocean & Civil Engn Shanghai 200240 Peoples R China|Shanghai Jiao Tong Univ State Key Lab Ocean Engn Shanghai 200240 Peoples R China|Shanghai Jiao Tong Univ Key Lab Hydrodynam Minist Educ Shanghai 200240 Peoples R China|Shanghai Jiao Tong Univ Shanghai Key Lab Digital Maintenance Bldg & Infra Shanghai 200240 Peoples R China;

    Shanghai Jiao Tong Univ Sch Naval Architecture Ocean & Civil Engn Shanghai 200240 Peoples R China|Shanghai Jiao Tong Univ State Key Lab Ocean Engn Shanghai 200240 Peoples R China;

    Shanghai Jiao Tong Univ Sch Naval Architecture Ocean & Civil Engn Shanghai 200240 Peoples R China|Shanghai Jiao Tong Univ State Key Lab Ocean Engn Shanghai 200240 Peoples R China|Shanghai Jiao Tong Univ Key Lab Hydrodynam Minist Educ Shanghai 200240 Peoples R China|Shanghai Jiao Tong Univ Shanghai Key Lab Digital Maintenance Bldg & Infra Shanghai 200240 Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Airfoil; Max lift-to-drag ratio; Gaussian process regression; Feature pool; Feature selection;

    机译:翼型;最大升力比率;高斯进程回归;特征池;特征选择;

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