首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THERMO-ACOUSTIC COMBUSTION INSTABILITY IN A LONGITUDINAL COMBUSTION CHAMBER: INFLUENCE OF THE GEOMETRY OF THE PLENUM
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NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THERMO-ACOUSTIC COMBUSTION INSTABILITY IN A LONGITUDINAL COMBUSTION CHAMBER: INFLUENCE OF THE GEOMETRY OF THE PLENUM

机译:纵向燃烧室中热声燃烧不稳定性的数值和实验研究:通风室几何形状的影响

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This paper concerns the study of self-sustained combustion instabilities that occur in a test rig characterized by a single longitudinal combustion chamber equipped with a full scale industrial burner and a longitudinal plenum. The length of both plenum and combustion chamber can be continuously varied. During tests, at a fixed value of the length of the combustion chamber, a sensibility of the amplitude of pressure oscillations to the length of the plenum has been registered, while the frequency remained constant. To investigate this behavior, a linear stability analysis has been performed evaluating the influence of the length of the plenum on the frequency and growth rate of the registered unstable mode. The analysis has been performed by means of a finite element method (FEM) code with a three-dimensional distribution of the n-t Flame Transfer Function (FTF) computed by means of computational fluid dynamics (CFD) simulations. According to the Rayleigh criterion, the distribution of the local Rayleigh index has been computed in order to evaluate the acoustic energy production, while the scattering matrix of the entire system has been used to evaluate the acoustic energy losses. Numerical results show that the reduction of the plenum length induces an increase of acoustic energy losses while the energy production remains almost constant. This result is in agreement with the reduction of the pressure oscillations amplitude observed during tests.
机译:本文涉及在以单个纵向燃烧室为特征的试验设备中发生的自持式燃烧不稳定性的研究,该纵向燃烧室配备了全尺寸工业燃烧器和纵向气室。气室和燃烧室的长度都可以连续变化。在测试过程中,以燃烧室长度的固定值记录了压力振荡幅度对气室长度的敏感性,而频率则保持恒定。为了研究此行为,进行了线性稳定性分析,评估了气室长度对所记录的不稳定模式的频率和增长率的影响。分析是通过有限元方法(FEM)代码进行的,其中n-t火焰传递函数(FTF)的三维分布是通过计算流体动力学(CFD)模拟计算得出的。根据瑞利准则,计算局部瑞利指数的分布以评估声能产生,而整个系统的散射矩阵已用于评估声能损失。数值结果表明,气室长度的减小引起声能损失的增加,而能量产生几乎保持恒定。该结果与在测试期间观察到的压力振荡幅度的减小是一致的。

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