首页> 外文会议>International symposium on air breathing engines;ISABE 2011 >EULER-LAGRANGE METHOD FOR NUMERICAL SIMULATION OF WATER DROPLET-LADEN COMPRESSOR FLOWS
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EULER-LAGRANGE METHOD FOR NUMERICAL SIMULATION OF WATER DROPLET-LADEN COMPRESSOR FLOWS

机译:载水滴压缩机流数值模拟的EULER-LAGRANGE方法

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To assure a safe operation of aero-engines in wet atmospheric conditions, the effects of water ingestion need to be fully understood and tested. In that point of interest the influence of water droplets on the flow characteristics in the compressor is mainly focused. Numerical simulation methods may be of great use in that case to examine in more detail the two-phase flow in compressor stages. Concerning this matter, a FORTRAN source code for the dispersed phase has been developed at the Laboratory of Turbo Machinery at the Helmut Schmidt University (University of the Federal Armed Forces), Germany, using the Euler-Lagrange method for the simulation of water droplet motion under high speed conditions with the continuous flow in turbo compressors. Implemented models consider droplet phenomena including turbulent dispersion, deformation, flow induced secondary breakup as well as splashing on wall surfaces. The source code communicates with ANSYS CFX 13.0 flow solver by the embedded user subroutine interface, at which readout of continuous phase data and input of disperse phase data using source terms is proceeded. In consequence fully coupled calculations are enabled by what the disperse phase may take influence on the flow pattern of the continuous phase. Due to the segregated computation the memory of the source code itself remains independent and offers advantages in modeling droplet breakup when memory may be dynamically allocated according to the numbers of droplets generated. Both the solver of the motion equations and the implemented models demonstrate their qualities in stability, efficiency and flexibility. In the test facility at the Laboratory a linear axial compressor cascade with water droplet loading has been investigated. For validation reasons the experiments were simulated numerically.
机译:为了确保航空发动机在潮湿的大气条件下安全运行,必须充分了解和测试吸水的影响。在该关注点上,主要集中于水滴对压缩机中流动特性的影响。在这种情况下,数值模拟方法可能会很有用,以更详细地检查压缩机级中的两相流。关于此问题,德国的赫尔穆特·施密特大学(联邦武装大学)的涡轮机械实验室已经开发了用于分散相的FORTRAN源代码,并使用Euler-Lagrange方法模拟了水滴运动。在高速条件下,涡轮压缩机不断流动。已实现的模型考虑了液滴现象,包括湍流扩散,变形,流动引起的二次破裂以及在壁表面的飞溅。源代码通过嵌入式用户子例程接口与ANSYS CFX 13.0流量求解器进行通信,在该接口上,可以进行连续相数据的读取和使用源项输入分散相数据的操作。结果,分散相可能对连续相的流型产生影响,从而可以进行完全耦合的计算。由于分开的计算,当可以根据生成的墨滴数量动态分配内存时,源代码本身的内存将保持独立,并在模拟墨滴破裂方面提供了优势。运动方程的求解器和已实现的模型都证明了其稳定性,效率和灵活性。在实验室的测试设备中,已经研究了带有水滴负载的线性轴向压缩机级联。出于验证的原因,对实验进行了数值模拟。

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