Benchmarking machine learning models against full-scale acoustic absorption measurements in gas turbine liners

Fuel Communications Pub Date : 2026-03-01 Epub Date: 2025-11-20 DOI:10.1016/j.jfueco.2025.100152
Abdullah Shahjalal, Roy Kalawsky, Demetrios Joannou, Faruk Ozdemir
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Abstract

Accurate prediction of acoustic energy absorption in gas turbine combustors is critical for enhancing performance, mitigating thermoacoustic instabilities, and reducing emissions. Traditional experimental and mathematical modeling approaches often struggle to capture the nonlinear and frequency-dependent behaviour of combustor liners, especially under varying operational conditions. This study presents a comprehensive evaluation of four machine learning (ML) models—Random Forest (RF), Extreme Gradient Boosting (XGB), Convolutional Neural Networks (CNN), and K-Nearest Neighbors (KNN)—against full-scale experimental measurements across six double-liner and three single-liner gas turbine configurations. A total of 615 operational records were used to train and validate model performance. In the double liner configuration, the RF and CNN models achieved the lowest average RMSE of 0.044, closely followed by XGB (0.045). However, XGB demonstrated the highest predictive accuracy (R² = 0.896), outperforming RF (0.891) and CNN (0.895), whose performance was partly constrained by limited dataset size. In the single liner configuration, XGB again delivered superior results (RMSE = 0.077, R² = 0.782) compared with RF (0.081, 0.580) and KNN (0.092, 0.470). The KNN model exhibited poor generalisation in the high-dimensional feature space, with R² dropping to 0.32 in certain tests. Overall, the machine learning framework reduced prediction error by approximately 31–56.2 % compared with conventional semi-empirical models (COS and COT), while requiring significantly lower computational effort to achieve comparable or superior accuracy. This is the first study to benchmark ML models against full-scale acoustic absorption data, introducing a validated data-driven framework with implications for combustor liner design, predictive maintenance, and real-time diagnostics. The integration of ML models into simulation workflows promises substantial reductions in experimental cost and improved design responsiveness. These findings offer a scalable, computationally efficient solution for aeroacoustic optimization—supporting the broader goal of cleaner, quieter, and more efficient gas turbine systems.
将机器学习模型与燃气轮机衬垫的全尺寸声吸收测量相比较
准确预测燃气轮机燃烧室的声能量吸收对提高性能、减轻热声不稳定性和减少排放至关重要。传统的实验和数学建模方法往往难以捕捉燃烧室衬套的非线性和频率依赖行为,特别是在不同的操作条件下。本研究对四种机器学习(ML)模型——随机森林(RF)、极端梯度增强(XGB)、卷积神经网络(CNN)和k近邻(KNN)——进行了全面的评估,并对六个双衬板和三个单衬板燃气轮机配置进行了全面的实验测量。总共使用了615个操作记录来训练和验证模型的性能。在双线性配置中,RF和CNN模型的平均RMSE最低,为0.044,XGB紧随其后(0.045)。然而,XGB表现出最高的预测精度(R²= 0.896),优于RF(0.891)和CNN(0.895),后者的性能在一定程度上受到数据集大小的限制。在单线性配置中,与RF(0.081, 0.580)和KNN(0.092, 0.470)相比,XGB再次提供了更好的结果(RMSE = 0.077, R²= 0.782)。KNN模型在高维特征空间中的泛化性较差,在某些测试中R²降至0.32。总体而言,与传统的半经验模型(COS和COT)相比,机器学习框架将预测误差降低了约31 - 56.2%,同时需要显着降低的计算工作量来达到相当或更高的精度。这是第一次将ML模型与全尺寸声吸收数据进行基准测试,引入了一个经过验证的数据驱动框架,该框架对燃烧室衬垫设计、预测性维护和实时诊断具有重要意义。将机器学习模型集成到仿真工作流程中可以大幅降低实验成本并提高设计响应能力。这些发现为气动声学优化提供了一个可扩展的、计算效率高的解决方案——支持更清洁、更安静、更高效的燃气轮机系统这一更广泛的目标。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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