Nonlinear flame response modelling by a parsimonious set of ordinary differential equations

Author:

Doehner Gregor1ORCID,Haeringer Matthias1ORCID,Silva Camilo F.1

Affiliation:

1. Thermo-Fluid Dynamics Group, School of Engineering and Design, Technical University of Munich, Garching, Germany

Abstract

In this work we present a parsimonious set of ordinary differential equations (ODEs) that describes with satisfactory precision the linear and non-linear dynamics of a typical laminar premixed flame in time and frequency domain. The proposed model is characterized by two ODEs of second-order that can be interpreted as two coupled mass-spring-damper oscillators with a symmetric, nonlinear damping term. This non-linear term is identified as function of the rate of displacement following [Formula: see text]. The model requires only four constants to be calibrated. This is achieved by carrying out an optimization procedure on one input and one output broadband signal obtained from high-fidelity numerical simulations (CFD). Note that the Transfer Function (FTF) or describing function (FDF) of the flame under investigation are not known a-priori, and therefore not used in the optimization procedure. Once the model is trained on CFD input and output time series, it is capable of recovering with quantitative accuracy the impulse response of the laminar flame under investigation and, hence, the corresponding frequency response (FTF). If fed with harmonic signals of different frequency and amplitude, the trained model is capable of retrieving with qualitative precision the flame describing function (FDF) of the studied flame. We show that the non-linear term [Formula: see text] is essential for capturing the gain saturation for high amplitudes of the input signal. All results are validated against CFD data.

Funder

Forschungsvereinigung Verbrennungskraftmaschinen e.V. FVV

Publisher

SAGE Publications

Subject

General Physics and Astronomy,Automotive Engineering,Energy Engineering and Power Technology

Reference25 articles.

1. Lieuwen T, Yang V (eds.) Combustion Instabilities in Gas Turbine Engines: Operational Experience, Fundamental Mechanisms and Modeling. Number v. 210 in Progress in Astronautics and Aeronautics. Reston, VA: American Institute of Aeronautics and Astronautics, 2005. ISBN 978-1-56347-669-3.

2. Prediction and control of combustion instabilities in real engines

3. Nonlinear self-excited oscillations of a ducted flame

4. A unified framework for nonlinear combustion instability analysis based on the flame describing function

5. Inclusion of higher harmonics in the flame describing function for predicting limit cycles of self-excited combustion instabilities

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3