Flow past a bluff body with a wavy stagnation face

被引:41
作者
Darekar, RM [1 ]
Sherwin, SJ [1 ]
机构
[1] Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2BY, England
关键词
D O I
10.1006/jfls.2000.0354
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Numerical investigations have been performed to study the flow past square-section cylinders with a spanwise geometric deformation leading to a stagnation face with a sinusoidal waviness. The computations were performed using a spectral/hp element solver over a range of Reynolds numbers from 10 to 500. Starting from fully developed shedding past a straight cylinder at a Reynolds number of 100, a sufficiently high waviness is impulsively introduced resulting in the stabilization of the the near-wake to a time-independent state. The steady nature of the near-wake is associated with a reduction in total drag of about 16% at a Reynolds number of 100 as compared with a straight, non-wavy cylinder. Further increases in the amplitude of the waviness lead to the emergence of hairpin vortices from the near-wake region, similar to the wake of a sphere at low Reynolds numbers. At higher Reynolds numbers, the drag reduction increases substantially, e.g. at a Reynolds number of 500 it is 34%, principally due to the increase in drag of the nonwavy cylinder. Alternative methods based on three-dimensional forms of bleed are investigated to suppress the von-Karman vortex street of a straight, non-wavy cylinder. (C) 2001 Academic Press.
引用
收藏
页码:587 / 596
页数:10
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