结合自相似性分析模型和人工神经网络,以数据驱动亚音速和超音速湍流喷流的传播预测

IF 5 Q2 ENERGY & FUELS
Gang Li , Rui Yang , Haisheng Zhen , Hu Wang , Haifeng Liu , Qinglong Tang , Mingfa Yao
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引用次数: 0

摘要

以往的湍流喷射火焰(TJF)自相似性分析模型在根据实验数据预测焰尖位置和速度方面存在固有的局限性。通过将已开发的自相似性分析模型与反向传播神经网络(BPNN)相结合,提出了一种预测亚音速和超音速 TJF 传播过程的新型模型(BP-TJF)。BP-TJF 模型根据初始温度、初始压力和氧气含量三个数据集进行训练。结果表明,亚音速喷气机的压差预测误差仅为 0.46%,超音速喷气机的压差预测误差为 5%。总体相关系数(R)和均方误差(MSE)分别为 0.95-0.97 和 0.01-0.1。通过遗传算法(GA)优化的模型大大提高了预测的稳定性。然而,在超压峰值预测方面仍有改进的余地。由于数据集尺度较小,射流传播自相似模型的参数误差较大,该模型无法实时反馈冲击波与火焰前沿之间的相互作用。从 BP-TJF 模型和实验中获得的喷流尖端位置和速度在大小和总体趋势上基本一致。在不考虑火焰结构的情况下,本文开发的预测框架可以计算出喷流尖端的传播特性,与实验和 CFD 的差异很小,这是一个很大的优势,尤其是在亚音速喷流的计算中。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Data-driven propagation prediction of subsonic and supersonic turbulent jets by combining self-similarity analysis model and artificial neural network

Previous self-similarity analysis models for turbulent jet flames (TJF) have inherent limitations in the flame tip location and velocity prediction based on experimental data. A novel model (BP-TJF) to predict the propagation process of subsonic and supersonic TJF is proposed by combining developed self-similarity analysis modeling and back propagation neural network (BPNN). The BP-TJF model is trained from three datasets of initial temperature, initial pressure, and oxygen content. The results show that the pressure difference prediction error was only 0.46 % for subsonic jets and 5 % for supersonic jets. The overall correlation coefficients (R) and mean squared errors (MSE) range from 0.95–0.97 and 0.01–0.1, respectively. The model optimized by genetic algorithm (GA) significantly improved the prediction stability. However, there is scope for improvement in the overpressure peak prediction. Due to the small-scale datasets and parameter errors of self-similar model for jet propagation, the model cannot provide real-time feedback on the interaction between the shock wave and the flame front. Jet tip locations and velocities obtained from the BP-TJF model and experiments are generally consistent in magnitude and overall trends. Without considering the flame structure, the prediction framework developed in this paper can calculate the jet tip propagation characteristics with little difference from experiments and CFD, which is a great advantage, especially in the calculation of subsonic jets.

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