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首页> 外文期刊>Journal of Propulsion and Power >Hybrid Reynolds-Averaged and Large-Eddy Simulation of Normal Injection into a Supersonic Crossflow
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Hybrid Reynolds-Averaged and Large-Eddy Simulation of Normal Injection into a Supersonic Crossflow

机译:正常向超声速横流中注入的混合雷诺平均和大涡模拟

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摘要

Injection through a circular port oriented normally to a Mach 1.6 crossflow is simulated using hybrid ReynoldsaveragednNavier–Stokes and large-eddy simulation turbulence models. The simulations compare the performance ofntwo related turbulence models. The standard formulation of the detached-eddy simulation equations is used in thencontext of a wall-modeled large-eddy simulation. A recently developed derivative of the detached-eddy simulationnformulation that was aimed at improving performance when operating as a wall-modeled large-eddy simulation isnalso used. These methods are used such that the large-scale turbulent structure of the flowfield can be resolved whilensimulating realistic Reynolds numbers. Simulations are performed on two grids to assess the influence of gridnresolution. Comparisons with flowfield visualizations from experiments are used to determine if the proper largescalenstructure is being resolved.Athorough validation of the results is performed by comparing with measurementsnof mean wall pressure from pressure-sensitive paint and measurements of mean velocity and turbulence intensitiesnfrom laser Doppler velocimetry. Results from the simulations are found to be in good agreement with the experiment.
机译:使用混合的ReynoldsaveragednNavier-Stokes模型和大涡流模拟湍流模型对通过通常面向1.6马赫错流的圆形端口进行注入进行了模拟。仿真比较了两个相关湍流模型的性能。然后,在壁面建模的大涡模拟中使用了分离涡模拟方程的标准公式。还使用了最近开发的分离涡流模拟公式的衍生物,该衍生物旨在在作为壁模型的大涡流模拟操作时提高性能。使用这些方法可以在模拟现实的雷诺数的同时解决流场的大规模湍流结构。在两个网格上执行仿真以评估网格分辨率的影响。通过与流场可视化结果进行比较来确定是否解决了合适的大型结构。通过与压敏涂料的平均壁压力测量值和激光多普勒测速仪的平均速度和湍流强度的测量值进行比较,对结果进行了充分的验证。仿真结果与实验非常吻合。

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