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Numerical Simulation of Twin Impinging Jets in a Cross-flow

机译:横流中双撞击射流的数值模拟

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摘要

When a vertical/short take-off and landing (VSTOL) aircraft is operated near the ground, a very complex flow field is created. This flow field can be represented by the configuration of twin impinging jets along the spanwise direction in a cross-flow. This paper presents a numerical study of this flow using the Reynolds Averaged Navier-Stokes (RANS) approach with a Reynolds Stress Model (RSM). The use of an RSM potentially offers a compromise between the computational efficiency of a k-ε model and the accuracy of a Large Eddy Simulation (LES). The current numerical results are validated against experimental data and the mean velocity profiles are reasonably well predicted by both the A-e model and the RSM with slightly better prediction by the RSM. However, the Reynolds stress prediction by the RSM is poor compared with the experimental data while LES does a much better job in this respect, indicating that to capture the unsteady flow features accurately LES is needed.
机译:当垂直/短距起降(VSTOL)飞机在地面附近运行时,会形成非常复杂的流场。该流场可以由在交叉流中沿翼展方向的双撞击射流的构造表示。本文使用雷诺应力模型(RSM)使用雷诺平均Navier-Stokes(RANS)方法对这种流动进行了数值研究。 RSM的使用可能会在k-ε模型的计算效率与大涡模拟(LES)的准确性之间做出折衷。目前的数值结果已针对实验数据进行了验证,A-e模型和RSM均合理地预测了平均速度曲线,而RSM则略好于预测。但是,与实验数据相比,RSM的雷诺应力预测效果较差,而LES在这方面做得更好,这表明需要准确捕获LES的不稳定流特征。

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