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Mach number prediction models based on Ensemble Neural Networks for wind tunnel testing

机译:基于Ensemble神经网络的马赫数预测模型用于风洞测试

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The 2.4m×2.4m wind tunnel is a system with the properties of strong nonlinear, multiple variables, serious coupling, large lagging, time-varying, etc. The complexity of all these phenomena makes the development of suitable dynamic Mach number models based on the aerodynamics laws very difficult. As an alternative, the Ensemble Neural Networks (ENN) model based on the feature subsets is proposed to address this problem. ENN built the sub-models on different lower dimension data sets, and reduced the complexity of the single Neural Networks (NN) built on the whole data set. Furthermore, a comparative study among the single NN models and the ENN models when used to predict the Mach number is conducted. Results show that the performance is improved by the ENN models. It is also shows that training time and testing time are much reduced by the ENN models.
机译:2.4m×2.4m风洞是一个具有强非线性,多变量,严重耦合,大滞后,时变等特性的系统。所有这些现象的复杂性使得基于该模型的动态马赫数模型的开发成为可能。空气动力学定律非常困难。作为替代方案,提出了基于特征子集的集成神经网络(ENN)模型来解决此问题。 ENN在不同的低维数据集上建立了子模型,并降低了在整个数据集上建立的单个神经网络(NN)的复杂性。此外,在用于预测马赫数的单个NN模型和ENN模型之间进行了比较研究。结果表明,ENN模型可以提高性能。这也表明,ENN模型大大减少了训练时间和测试时间。

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