The resilience of the logarithmic law to pressure gradients: evidence from direct numerical simulation

被引:23
作者
Johnstone, Roderick [1 ]
Coleman, Gary N. [1 ]
Spalart, Philippe R. [2 ]
机构
[1] Univ Southampton, Sch Engn Sci, Southampton SO17 1BJ, Hants, England
[2] Boeing Commercial Airplanes, Seattle, WA 98124 USA
基金
英国工程与自然科学研究理事会;
关键词
modelling; simulation; turbulent flows; TURBULENT-BOUNDARY-LAYER; FLOW; VELOCITY;
D O I
10.1017/S0022112009992333
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Wall-bounded turbulence in pressure gradients is studied using direct numerical simulation (DNS) of a Couette-Poiseuille now. The motivation is to include adverse pressure gradients, to complement the favourable ones present in the well-studied Poiseuille flow, and the central question is how the scaling laws react to a gradient in the total shear stress or equivalently to a pressure gradient. In the case considered here, the ratio of local stress to wall stress, namely tau(+), ranges from roughly 2/3 to 3/2 in the 'wall region'. By this we mean the layer believed not to be influenced by the opposite wall and therefore open to simple, universal behaviour. The normalized pressure gradients p(+) equivalent to d tau(+)/dy(+) at the two walls are -0.00057 and +0.0037. The outcome is in broad agreement with the findings of Galbraith, Sjolander & Head (Aeronaut. Quart. vol. 27, 1977, pp. 229-242) relating to boundary layers (based on measured profiles): the logarithmic velocity profile is much more resilient than two other, equally plausible assumptions, namely universality of the mixing length l = ky and that of the eddy viscosity nu(t) = u(tau)ky. In pressure gradients, with tau(+) not equal 1, these three come into conflict, and our primary purpose is to compare them. We consider that the Karman constant k is unique but allow a range from 0.38 to 0.41, consistent with the current debates. It makes a minor difference in the interpretation. This finding of resilience appears new as a DNS result and is free of the experimental uncertainty over skin friction. It is not as distinct in the (rather strong) adverse gradient as it Is in the favourable one; for instance the velocity U(+) at y(+) = 50 is lower by 3% on the adverse gradient side. A plausible cause is that the wall shear stress is small and somewhat overwhelmed by the stress and kinetic energy in the bulk of the flow. The potential of a correction to the 'law of the wall' based purely on p(+) is examined, with mixed results. We view the preference for the log law as somewhat counter-intuitive in that the scaling law is non-local but also as becoming established and as highly relevant to turbulence modelling.
引用
收藏
页码:163 / 175
页数:13
相关论文
共 19 条
[1]  
[Anonymous], AERONAUT Q
[2]  
[Anonymous], 45 AIAA AER SCI M EX
[3]  
BLACKWELL BF, 1972, HMT16 STANDF U MECH
[4]   THE LAW OF THE WALL IN TURBULENT-FLOW [J].
BRADSHAW, P ;
HUANG, GP .
PROCEEDINGS OF THE ROYAL SOCIETY-MATHEMATICAL AND PHYSICAL SCIENCES, 1995, 451 (1941) :165-188
[5]  
ELTELBANY MMM, 1980, J FLUID MECH, V100, P1, DOI 10.1017/S0022112080000973
[6]   EDDY VISCOSITY AND MIXING LENGTH FROM MEASURED BOUNDARY-LAYER DEVELOPMENTS [J].
GALBRAITH, RAM ;
HEAD, MR .
AERONAUTICAL QUARTERLY, 1975, 26 (MAY) :133-154
[7]  
HEAD MR, 1975, AERONAUT Q, V27, P229
[8]   Scaling of the velocity fluctuations in turbulent channels up to Reτ=2003 -: art. no. 011702 [J].
Hoyas, S ;
Jiménez, J .
PHYSICS OF FLUIDS, 2006, 18 (01)
[9]   IMPROVEMENTS TO A NONEQUILIBRIUM ALGEBRAIC TURBULENCE MODEL [J].
JOHNSON, DA ;
COAKLEY, TJ .
AIAA JOURNAL, 1990, 28 (11) :2000-2003
[10]   TURBULENCE STATISTICS IN FULLY-DEVELOPED CHANNEL FLOW AT LOW REYNOLDS-NUMBER [J].
KIM, J ;
MOIN, P ;
MOSER, R .
JOURNAL OF FLUID MECHANICS, 1987, 177 :133-166