LOW-REYNOLDS-NUMBER-K-EPSILON MODEL FOR UNSTEADY TURBULENT BOUNDARY-LAYER FLOWS

被引:72
作者
FAN, SX [1 ]
LAKSHMINARAYANA, B [1 ]
BARNETT, M [1 ]
机构
[1] UNITED TECHNOL CORP,RES CTR,E HARTFORD,CT 06108
基金
美国国家航空航天局;
关键词
D O I
10.2514/3.11849
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
An assessment of the near-wall and low-Reynolds-number functions used in low-Reynolds-number k-epsilon models suggests that they are not suitable for the near-wall region of unsteady turbulent boundary layers, where the flow is characterized by rapid changes in phase. An improved low-Reynolds-number k-epsilon model is developed in this paper. The near-wall and low-Reynolds-number functions in this model are formulated as functions of the local turbulent Reynolds numbers instead of the inner variable y+. The present model also has the correct asymptotic behavior in the near-wall region. The turbulence model has been incorporated in an unsteady boundary-layer code and validated for unsteady turbulent boundary layers with and without adverse pressure gradients. The predictions agree well with the experimental data and the theoretical analysis. For the cases tested, the present model correctly predicts the unsteady near-wall now and the unsteady skin friction at various frequencies.
引用
收藏
页码:1777 / 1784
页数:8
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