首页> 外文期刊>Journal of propulsion and power >Simplified Description of Heat Release Oscillations for Assessing Combustor Stability
【24h】

Simplified Description of Heat Release Oscillations for Assessing Combustor Stability

机译:放热振荡的简化描述,用于评估燃烧室的稳定性

获取原文
获取原文并翻译 | 示例
       

摘要

A simplified description of heat release oscillations associated with vortex-driven combustion instabilities is developed that can greatly reduce the amount of data required for determining the linear stability of combustor eigenmodes. The simplification is achieved by first representing heat release fluctuations as sinusoidal oscillations and then modeling the amplitude of the oscillations using a heuristic assumption of proportionality between the mean and the fluctuating components of local heat release. It is shown that by simply knowing 1) the average heat release, and 2) the heat release at any particular phase of the oscillations, complete spatiotemporal description of heat release oscillations can be reconstructed, and the linear stability of a given eigenmode can be determined. The description is shown to correctly determine the linear stability of a 150 Hz vortex-driven marginal amplitude instability in a laboratory-scale dump combustor with local and global Rayleigh indices within 16% of the experimentally obtained values. The approach opens up the possibility of predicting modal stability in the future without experiments, by using other forms of data, such as computational data on time-averaged heat release distribution and physics-based modeling data on phase-specific heat release rates.
机译:发展了与涡流驱动的燃烧不稳定性相关的放热振荡的简化描述,它可以大大减少确定燃烧器本征模式线性稳定性所需的数据量。通过首先将热量释放波动表示为正弦振荡,然后使用均值和局部热量释放的波动分量之间的比例启发法假设来模拟振荡的幅度,从而实现简化。结果表明,通过简单地知道1)平均放热,和2)在振荡的任何特定相位的放热,就可以重建放热振荡的完整时空描述,并且可以确定给定本征模的线性稳定性。说明可以正确确定实验室规模的倾卸式燃烧室中150 Hz涡流驱动的边际幅度不稳定性的线性稳定性,其局部和全局瑞利指数在实验获得的值的16%以内。通过使用其他形式的数据,例如时间平均放热分布的计算数据和特定于相的放热速率的基于物理的建模数据,该方法提供了无需进行实验即可预测未来模态稳定性的可能性。

著录项

  • 来源
    《Journal of propulsion and power》 |2019年第1期|152-158|共7页
  • 作者

    Park S.; Ghosh A.; Yu K. H.;

  • 作者单位

    Univ Maryland, Aerosp Engn Dept, College Pk, MD 20742 USA;

    Univ Maryland, Aerosp Engn Dept, College Pk, MD 20742 USA;

    Univ Maryland, Aerosp Engn Dept, College Pk, MD 20742 USA;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号