Artificial neural network analysis of the Nusselt number and friction factor of hydrocarbon fuel under supercritical pressure

IF 5.4 2区 工程技术 Q1 ENGINEERING, AEROSPACE Propulsion and Power Research Pub Date : 2022-09-01 DOI:10.1016/j.jppr.2022.08.002
Kaihang Tao, Jianqin Zhu, Zeyuan Cheng, Dike Li
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引用次数: 3

Abstract

This paper presents the Nusselt number and friction factor model for hydrocarbon fuel under supercritical pressure in horizontal circular tubes using an artificial neural network (ANN) analysis on the basis of the back propagation algorithm. The derivation of the proposed model relies on a large number of experimental data obtained from the tests performed with the platform of supercritical flow and heat transfer. Different topology structures, training algorithms and transfer functions are employed in model optimization. The performance of the optimal ANN model is evaluated with the mean relative error, the determination coefficient, the number of iterations and the convergence time. It is demonstrated that the model has high prediction accuracy when the tansig transfer function, the Levenberg-Marquardt training algorithm and the three-layer topology of 4-9-1 are selected. In addition, the accuracy of the ANN model is observed to be the highest compared with other classic empirical correlations. Mean relative error values of 4.4% and 3.4% have been achieved for modeling of the Nusselt number and friction factor respectively over the whole experimental data set. The ANN model established in this paper is shown to have an excellent performance in learning ability and generalization for characterizing the flow and heat transfer law of hydrocarbon fuel, which can provide an alternative approach for the future study of supercritical fluid characteristics and the associated engineering applications.

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超临界压力下烃类燃料努塞尔数和摩擦因数的人工神经网络分析
本文采用基于反向传播算法的人工神经网络(ANN)分析方法,建立了水平圆管内超临界压力下碳氢燃料的努塞尔数和摩擦因子模型。该模型的推导依赖于在超临界流动和传热平台上进行的大量实验数据。模型优化采用了不同的拓扑结构、训练算法和传递函数。用平均相对误差、确定系数、迭代次数和收敛时间来评价最优人工神经网络模型的性能。结果表明,当选择tansig传递函数、Levenberg-Marquardt训练算法和4-9-1的三层拓扑结构时,该模型具有较高的预测精度。此外,与其他经典经验相关性相比,人工神经网络模型的准确性最高。在整个实验数据集上,Nusselt数和摩擦系数的平均相对误差分别为4.4%和3.4%。本文所建立的人工神经网络模型在表征烃类燃料流动和传热规律方面具有良好的学习能力和泛化能力,可为今后超临界流体特性的研究及相关工程应用提供一种替代方法。
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来源期刊
CiteScore
7.50
自引率
5.70%
发文量
30
期刊介绍: Propulsion and Power Research is a peer reviewed scientific journal in English established in 2012. The Journals publishes high quality original research articles and general reviews in fundamental research aspects of aeronautics/astronautics propulsion and power engineering, including, but not limited to, system, fluid mechanics, heat transfer, combustion, vibration and acoustics, solid mechanics and dynamics, control and so on. The journal serves as a platform for academic exchange by experts, scholars and researchers in these fields.
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