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Use of Active Learning to Design Wind Tunnel Runs for Unsteady Cavity Pressure Measurements

机译:利用主动学习设计用于不稳定腔压力测量的风洞运行

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摘要

Wind tunnel tests to measure unsteady cavity flow pressure measurements can be expensive, lengthy, and tedious. In this work, the feasibility of an active machine learning technique to design wind tunnel runs using proxy data is tested. The proposed active learning scheme used scattered data approximation in conjunction with uncertainty sampling (US). We applied the proposed intelligent sampling strategy in characterizing cavity flow classes at subsonic and transonic speeds and demonstrated that the scheme has better classification accuracies, using fewer training points, than a passive Latin Hypercube Sampling (LHS) strategy.
机译:用于测量非稳态空腔流量压力测量的风洞测试可能很昂贵,冗长且繁琐。在这项工作中,测试了一种主动机器学习技术来使用代理数据设计风洞运行的可行性。拟议的主动学习方案将离散数据近似与不确定性采样(US)结合使用。我们将拟议的智能采样策略应用于以亚音速和跨音速速度表征腔流类别,并证明了该方案与被动拉丁超立方体采样(LHS)策略相比,具有更少的训练点,具有更好的分类精度。

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  • 来源
    《International journal of aerospace engineering》 |2014年第2014期|218710.1-218710.11|共11页
  • 作者单位

    Mechanical Engineering and Material Science Department, William Marsh Rice University, Houston, TX 77251-1892, USA;

    Mechanical Engineering and Material Science Department, William Marsh Rice University, Houston, TX 77251-1892, USA;

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  • 正文语种 eng
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