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湍流模型对喷流计算精度的影响研究(英文)
引用本文:唐志共,刘刚,牟斌,黄勇. 湍流模型对喷流计算精度的影响研究(英文)[J]. 空气动力学学报, 2010, 28(2)
作者姓名:唐志共  刘刚  牟斌  黄勇
作者单位:1. 西北工业大学航空学院,陕西,西安,710072
2. 中国空气动力研究与发展中心,四川,绵阳,621000
摘    要:采用三维RANS代码MBNS3D对包含了内流、外流及后体干扰的三种简化尾喷流,进行了数值模拟研究。通过壁面压力分布及喷流截面速度型与实验数据的对比,研究了SA和SST两种湍流模型及其修正(SACC,SADES,SSTCC)对喷流计算精度的影响。本文计算表明,SSTCC模拟效果最为精确;利用SA模型进行脱体涡模拟,在同样的网格下优势不明显。湍流模型可压缩修正改善了模拟喷流的膨胀趋势,但对附面层分离位置的预测,在本文的工作中,还不如原始模型。两类模型相比,SST模型的结果好于SA模型。

关 键 词:喷流  RANS方程  湍流模型  

Effects of turbulence models on the numerical simulation of nozzle jets
TANG Zhi-gong,LIU Gang,MOU Bin,HUANG Yong. Effects of turbulence models on the numerical simulation of nozzle jets[J]. Acta Aerodynamica Sinica, 2010, 28(2)
Authors:TANG Zhi-gong  LIU Gang  MOU Bin  HUANG Yong
Affiliation:1.Northwestern Ploytechnical University/a>;Xi'an 710072/a>;China/a>;2.China Aerodynamic Research and Development Center/a>;Mianyang 621000/a>;China
Abstract:Three different jet flows, which characterized by internal flow, internal and external mixing flow and after-body interference, were simulated numerically with the three-dimensional Reynolds Averaged Navier-Stokes code MBNS3D.These simulations are focused on the effects of two representative turbulence models (the S-A and the k-ω SST model) and their compressibility correction schemes on some typical nozzle flows.Wall pressure distribu-tion and jet velocity profile are compared with experimental data.Results show that better agreement can be obtained in nozzle flow simulations with the k-ω SST model and its compressibility correction, and the advantage of the S-A detached eddy simulation is not remarkable on the same grid compared simulation with the S-A model.
Keywords:jet  Reynolds averaged N-S equations  turbulence model  
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