Experimental investigation of the log-law for an adverse pressure gradient turbulent boundary layer flow at Reθ up to 10000

被引:0
|
作者
Knopp, T. [1 ]
Schanz, D. [1 ]
Schroeder, A. [1 ]
Dumitra, M. [2 ]
Kaehler, C. J. [2 ]
机构
[1] DLR German Aerosp Ctr, Inst Aerodynam & Flow Technol, Bunsenstr 10, D-37073 Gottingen, Germany
[2] Univ Bundeswehr Munchen UniBw, Inst Fluid Mech & Aerodynam, D-85577 Neubiberg, Germany
关键词
WALL; SEPARATION;
D O I
10.1615/ICHMT.2012.ProcSevIntSympTurbHeatTransfPal.510
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
We present an experimental investigation of a turbulent boundary layer flow at a significant adverse pressure gradient at Reynolds number Re-theta up to 10000 using large field PIV. The testcase is designed to start from a zero pressure gradient flow at Re-theta approximate to 8000 with a distinct log-law region following a slowly rising adverse pressure gradient. This allows to reveal a breakdown of the log-law under the effect of the adverse pressure gradient. The region described by the log law is progressively reduced in terms of y(+) and then joins into a modified log-law which gives a good fit to the data up to at least y/delta(99) approximate to 0.2.
引用
收藏
页码:457 / 468
页数:12
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