首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Time-Domain Bloch Boundary Conditions for Efficient Simulation of Thermoacoustic Limit Cycles in (Can-)Annular Combustors
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Time-Domain Bloch Boundary Conditions for Efficient Simulation of Thermoacoustic Limit Cycles in (Can-)Annular Combustors

机译:(Can-)环形燃烧室热声极限循环的高效时域Bloch边界条件

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摘要

Thermo-acoustic eigenmodes of annular or can-annular combustion chambers, which typically feature a discrete rotational symmetry, may be computed in an efficient manner by utilizing the Bloch-wave theory. Unfortunately, the application of the Bloch-wave theory to combustion dynamics has hitherto been limited to the frequency domain. In this study, we present a time-domain formulation of Bloch boundary conditions (BBC), which allows to employ them in time domain simulations, e.g., computational fluid dynamics (CFD) simulations. The BBCs are expressed as acoustic scattering matrices and translated to complex-valued state-space systems. In a hybrid approach an unsteady, compressible CFD simulation of the burner-flame zone is coupled via characteristic-based state-space boundary conditions to a reduced order model of the combustor acoustics that includes BBCs. The acoustic model with BBC accounts for cross-can acoustic coupling and the discrete rotational symmetry of the configuration, while the CFD simulation accounts for the nonlinear flow-flame acoustic interactions. This approach makes it possible to model limit cycle oscillations of (can-)annular combustors at drastically reduced computational cost compared to CFD simulations of the full configuration and without the limitations of weakly nonlinear approaches that utilize a flame describing function. In this study, the suggested approach is applied to a generic multican combustor. Results agree well with a fully compressible CFD simulation of the complete configuration.
机译:可以利用布洛赫波理论以有效的方式来计算通常具有离散旋转对称性的环形或环形燃烧室的热声本征模式。不幸的是,迄今为止,布洛赫波理论在燃烧动力学中的应用仅限于频域。在这项研究中,我们提出了Bloch边界条件(BBC)的时域公式,可将其用于时域仿真中,例如计算流体动力学(CFD)仿真。 BBC表示为声散射矩阵,并转换为复数值状态空间系统。在混合方法中,燃烧器火焰区域的不稳定,可压缩的CFD模拟通过基于特征的状态空间边界条件耦合到包含BBC的燃烧器声学降阶模型。具有BBC的声学模型考虑了跨罐声学耦合和配置的离散旋转对称性,而CFD模拟则考虑了非线性的流-火焰声学相互作用。与完全配置的CFD模拟相比,这种方法可以以大大降低的计算成本对(can)环形燃烧室的极限循环振荡进行建模,而不受使用火焰描述功能​​的弱非线性方法的限制。在这项研究中,建议的方法应用于通用的多罐燃烧器。结果与完整配置的完全可压缩CFD模拟非常吻合。

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