论文标题
耗散的喷嘴中的组成噪声
Compositional noise in nozzles with dissipation
论文作者
论文摘要
我们提出了一个物理模型,以预测通过粘性耗散(非分散喷嘴)在喷嘴中成分不均匀性加速产生的间接噪声。首先,我们从多组分流的保护定律中得出了准二维方程。其次,我们使用文献中可用于四种气体的二元混合物的实验数据验证了所提出的模型。第三,我们计算出具有/没有冲击波的亚音速和超音速流中不同Helmholtz数量和摩擦因子的喷嘴传输函数。我们表明,摩擦对间接噪声的产生有重大影响,该噪声识别和解释了物理机制。第四,我们找到了具有路径积分的半分析溶液,该溶液可提供相对于Helmholtz数的渐近扩展。第五,我们介绍了组成噪声缩放系数,该系数仅适用于仅了解一个单组分气体传递函数的知识来快速估计组成噪声。近似错误小于$ 1 \%$。提出的低阶模型提供了对多组分气体间接噪声的转移函数的准确估计和物理洞察力。这为燃气轮机的准确预测和理解发电的新可能性打开了新的可能性。
We propose a physical model to predict indirect noise generated by the acceleration of compositional inhomogeneities in nozzles with viscous dissipation (non-isentropic nozzles). First, we derive the quasi-one-dimensional equations from the conservation laws of multicomponent flows. Second, we validate the proposed model with the experimental data available in the literature for binary mixtures of four gases. Third, we calculate the nozzle transfer functions for different Helmholtz numbers and friction factors, in both subsonic and supersonic flows with/without shock waves. We show that friction has a significant effect on the generation of indirect noise, for which the physical mechanism is identified and explained. Fourth, we find a semi-analytical solution with path integrals, which provide an asymptotic expansion with respect to the Helmholtz number. Fifth, we introduce the compositional noise scaling factor, which is applied to quickly estimate compositional noise from the knowledge of only one single-component gas transfer function. The approximation error is less than $1\%$. The proposed low-order model provides accurate estimates of the transfer functions and physical insight into indirect noise for multicomponent gases. This opens up new possibilities to accurately predict, and understand, sound generation in gas turbines.