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

机译:基于集体神经网络的风洞测试马赫数预测模型

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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风洞是一个具有强度非线性,多个变量,严重耦合,大滞后,时变等的系统的系统。所有这些现象的复杂性都是基于的合适动态马赫数模型的发展。空气动力学法则非常困难。作为替代方案,提出了基于特征子集的集合神经网络(ENN)模型来解决这个问题。 ENN在不同的较低尺寸数据集上构建了子模型,并降低了在整个数据集上构建的单个神经网络(NN)的复杂性。此外,进行了用于预测马赫数的单个NN模型和ENN模型之间的比较研究。结果表明,enn模型的性能得到改善。还显示enn模型的训练时间和测试时间大大降低。

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