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Comparison of CFD Predictions and Experimental Measurements of Liquid Jet Injection into a Vitiated Crossflow

机译:CFD预测值和液体喷射流向垂直流的比较

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This paper describes an exercise carried out to establish the capability of time efficient CFD based simulations to describe the injection of fuel from a plain jet into a crossflow. The exercise provides a quantitative assessment of the accuracy with which simulation tools can predict spray plume trajectory, dispersion, droplet size and velocity. The effort involved collection of detailed data associated with a spray plume produced by Jet-A injected from a plain jet into a high speed crossflow at 1000 deg K. A document outlining the details of the inlet and boundary conditions needed to set up the CFD solution was provided to seven participants which represented gas turbine manufacturers, CFD vendors, research firms, and component providers. These participants provided at least one simulation of the problem posed. The participants were given 6 weeks to complete the exercise and return the results to ERC which then carried out the detailed comparison of the results with the experimental data. Penetration height, plume width, volume flux, and integrated volume flux were compared at two downstream axial locations. D_(32) and average spray axial velocity are compared amongst the CFD results. The results shown herein emphasize the characteristics of the spray plume (i.e., penetration and plume width) and indicate (1) a wide range in the simulation results and (2) generally marginal agreement with the experimental results. For example, the penetration 1" downstream was overestimated by 53% on average and width overpredicted by 111%. No dominant trend relative to modeling approach and overall agreement with the measured results was found. As a result, it is difficult to derive a "best practice" recommendation relative successful application of the modeling approaches evaluated in this study.
机译:本文描述了一项练习,该练习旨在建立基于时间高效CFD的仿真功能,以描述从普通喷嘴向错流喷射燃料的过程。该练习提供了对准确性的定量评估,仿真工具可利用该准确性来预测喷雾羽的轨迹,分散,液滴大小和速度。这项工作涉及收集与从普通喷气机注入1000度K的高速横流的Jet-A产生的喷射羽流相关的详细数据。一份文件概述了设置CFD解决方案所需的入口和边界条件的详细信息提供给代表燃气轮机制造商,CFD供应商,研究公司和组件提供商的七名参与者。这些参与者至少提出了一个模拟问题。给参与者6周的时间来完成练习并将结果返回给ERC,ERC然后将结果与实验数据进行详细的比较。在两个下游轴向位置比较了渗透高度,羽流宽度,体积通量和积分体积通量。在CFD结果中比较了D_(32)和平均喷雾轴向速度。本文显示的结果强调了喷雾羽流的特性(即渗透和羽流宽度),并指出(1)模拟结果的范围很广,以及(2)与实验结果的边际一致性。例如,下游的渗透“平均”高估了53%,而宽度的高估了111%。相对于建模方法和与测量结果的总体一致性,没有发现主导趋势。因此,很难得出“最佳做法”建议在本研究中评估建模方法的相对成功应用。

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