Reθt转捩模型中两输运方程的简化得到一方程转捩预测模型。将其与SST湍流模型进行耦合并利用Schubauer and Klebanoff平板标定各参数。此外,经过分析SST与SA湍流模型输运方程间的联系,修正SA湍流模型中的ft2函数,通过其对源项的控制实现文中一方程转捩预测模型与SA湍流模型的耦合。最后,利用得到的分别基于SST和SA的一方程转捩预测模型对S809低速翼型、DLR-F5机翼进行数值模拟。结果表明:由S809翼型的计算数据可得出文中构建的一方程转捩模型在线性区与实验数据吻合很好,力系数在8°迎角范围内均达到了3%以内的预测精度;DLR-F5机翼在中翼段和外翼段的转捩预测位置与实验较接近,吻合良好。2个算例均表明改进后的一方程转捩模型取得了良好的预测效果。"/> Reθt转捩模型中两输运方程的简化得到一方程转捩预测模型。将其与SST湍流模型进行耦合并利用Schubauer and Klebanoff平板标定各参数。此外,经过分析SST与SA湍流模型输运方程间的联系,修正SA湍流模型中的ft2函数,通过其对源项的控制实现文中一方程转捩预测模型与SA湍流模型的耦合。最后,利用得到的分别基于SST和SA的一方程转捩预测模型对S809低速翼型、DLR-F5机翼进行数值模拟。结果表明:由S809翼型的计算数据可得出文中构建的一方程转捩模型在线性区与实验数据吻合很好,力系数在8°迎角范围内均达到了3%以内的预测精度;DLR-F5机翼在中翼段和外翼段的转捩预测位置与实验较接近,吻合良好。2个算例均表明改进后的一方程转捩模型取得了良好的预测效果。" />
论文:2016,Vol:34,Issue(3):404-410
引用本文:
徐晓娟, 白俊强, 史亚云. 基于当地变量的一方程转捩预测模型[J]. 西北工业大学学报
Xu Xiaojuan, Bai Junqiang, Shi Yayun. A One-Equation Transition Model Based on Local Variables[J]. Northwestern polytechnical university

基于当地变量的一方程转捩预测模型
徐晓娟, 白俊强, 史亚云
西北工业大学 航空学院, 陕西 西安 710072
摘要:
引入适用于边界层内的湍流度及压力梯度因子求解公式,构造Reθc和Flength经验关系式,实现对γ-Reθt转捩模型中两输运方程的简化得到一方程转捩预测模型。将其与SST湍流模型进行耦合并利用Schubauer and Klebanoff平板标定各参数。此外,经过分析SST与SA湍流模型输运方程间的联系,修正SA湍流模型中的ft2函数,通过其对源项的控制实现文中一方程转捩预测模型与SA湍流模型的耦合。最后,利用得到的分别基于SST和SA的一方程转捩预测模型对S809低速翼型、DLR-F5机翼进行数值模拟。结果表明:由S809翼型的计算数据可得出文中构建的一方程转捩模型在线性区与实验数据吻合很好,力系数在8°迎角范围内均达到了3%以内的预测精度;DLR-F5机翼在中翼段和外翼段的转捩预测位置与实验较接近,吻合良好。2个算例均表明改进后的一方程转捩模型取得了良好的预测效果。
关键词:    转捩预测模型    湍流模型    层流边界层    数值分析    标定   
A One-Equation Transition Model Based on Local Variables
Xu Xiaojuan, Bai Junqiang, Shi Yayun
College of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China
Abstract:
In order to simplify the transition model by substituting two equations with one,the local turbulence intensity and pressure gradient parameter are introduced to construct the new empirical correlations for Reθc and Flength. The new model can be coupled with SST turbulence model, whose parameters are calibrated by the Schubauer and Klebanoff flat plate. Furthermore, by analyzing the relations of transport equations between SST and SA, ft2 function, a part of the source terms, is corrected to realize the coupling of one equation transition model and SA turbulence model. Finally, numerical analysis are conducted on S809 airfoil and DLR F5 wing, and the results indicate that: simulations using one-equation transition models agree well with experiments in linear region, and the error of force coefficients is less than 3% for S809 foil; for DLR-F5 wing, the transition locations also meet well with the experiments except for the root part. Both of the cases demonstrate that the polished model performs quite accurately in the prediction of transition.
Key words:    transition prediction model    turbulence models    laminar boundary layer    numerical analysis    calibration   
收稿日期: 2015-10-27     修回日期:
DOI:
基金项目: 国家"973"计划(2014CB744804)资助
通讯作者:     Email:
作者简介: 徐晓娟(1991—),女,西北工业大学硕士研究生,主要从事转捩数值模拟方法及粗糙带研究。
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