NEAR-WALL RESPONSE IN TURBULENT SHEAR FLOWS SUBJECTED TO IMPOSED UNSTEADINESS

被引:24
作者
MANKBADI, RR
LIU, JTC
机构
[1] BROWN UNIV, DIV ENGN, PROVIDENCE, RI 02912 USA
[2] LAB AEROTHERM, CNRS, F-92190 MEUDON, FRANCE
关键词
D O I
10.1017/S0022112092001630
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Rapid-distortion theory is adapted to introduce a truly unsteady closure into a simple phenomenological turbulence model in order to describe the unsteady response of a turbulent wall layer exposed to a temporarily oscillating pressure gradient. The closure model is built by taking the ratio of turbulent shear stress to turbulent kinetic energy to be a function of the effective strain. The latter accounts for the history of the flow. The computed unsteady velocity fluctuations and modulated turbulent stresses compare favourably in the 'non-quasi-steady' frequency range, where quasi-steady assumptions would fail. This suggests that the concept of rapid distortion is especially appropriate for unsteady flows. This paper forms the basis for acoustical studies of the problem to be reported elsewhere.
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收藏
页码:55 / 71
页数:17
相关论文
共 43 条
[1]   INTERACTIONS BETWEEN LARGE-SCALE STRUCTURE AND FINE-GRAINED TURBULENCE IN A FREE SHEAR-FLOW .2. DEVELOPMENT OF SPATIAL INTERACTIONS IN MEAN [J].
ALPER, A ;
LIU, JTC .
PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 1978, 359 (1699) :497-523
[2]  
Betchov R., 1967, STABILITY PARALLEL F
[3]  
BINDER G, 1981, UNSTEADY TURBULENT S, P100
[4]  
BINDER G, 1985, 5TH S TURB SHEAR FLO
[5]   CALCULATION OF BOUNDARY-LAYER DEVELOPMENT USING TURBULENT ENERGY EQUATION [J].
BRADSHAW, P ;
FERRISS, DH ;
ATWELL, NP .
JOURNAL OF FLUID MECHANICS, 1967, 28 :593-+
[6]  
CARR LW, 1981, UNSTEADY TURBULENT S, P3
[7]  
COOK WJ, 1985, 5TH S TURB SHEAR FLO
[8]  
COUSTEIX J, 1986, ANNU REV FLUID MECH, V18, P173
[9]  
COUSTEIX J, 1981, UNSTEADY TURBULENT S, P120
[10]   BEHAVIOR OF THE TURBULENT ENERGY EQUATION AT A FIXED BOUNDARY [J].
DERKSEN, RW ;
AZAD, RS .
AIAA JOURNAL, 1981, 19 (02) :238-239