THE RESPONSE OF A TURBULENT BOUNDARY-LAYER TO ARTIFICIAL DISTURBANCES

被引:0
|
作者
BRAND, AJ [1 ]
VOLLEBREGT, HJM [1 ]
WEMMERS, AK [1 ]
NIEUWSTADT, FTM [1 ]
机构
[1] DELFT UNIV TECHNOL, AERODYNAM & HYDRODYNAM LAB, 2628 AL DELFT, NETHERLANDS
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TH [机械、仪表工业];
学科分类号
0802 ;
摘要
With periodic fluid injection through small slots, a turbulent boundary layer is artificially disturbed on scales that are of the order of those of the natural quasi-periodic events. The periodic phase-average of the streamwise fluid velocity is determined from hot-film measurements, and used to find the coherent velocity component as defined by the triple decomposition. It appears that, when a disturbance is active, the generated flow pattern is very similar to the one caused by the interaction of a crossflow and a jet. However, when it is terminated, the turbulent boundary layer returns to its undisturbed state.
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页码:193 / 202
页数:10
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