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This paper presents an extensive numerical study of 3-D laminar flow around two wavy cylinders in the tandem arrangement for spacing ratios(/)m L D ranging from 1.5 to 5.5 at a low Reynolds number of 100.The investigation focuses on the effects of spacing ratio(/)m L D and wavy surface on the 3-D near wake flow patterns,the force and pressure coefficients and the vortex shedding frequency for the two tandem wavy cylinders.Flows around the two tandem circular cylinders are also obtained for comparison.With the spacing ratio in the range of/=1.5-5.5m L D,unlike two tandem circular cylinders,the wavy cylinders in the tandem arrangement do not have the wake interference behaviour of three basic types.The vortex shedding behind the upstream wavy cylinder occurs at a further downstream position as compared with that of the upstream circular cylinder.This leads to the weakening of the effect of the vibration of the cylinders as well as a distinct drag reduction.The effects of the drag reduction and the control of the vibration of the two wavy cylinders in tandem become more and more evident when/m L D 4.0,with a distinct vortex shedding in the upstream cylinder regime for the two circular cylinders in tandem.
This paper presents an extensive numerical study of 3-D laminar flow around two wavy cylinders in the tandem arrangement for spacing ratios (/) m LD ranging from 1.5 to 5.5 at a low Reynolds number of 100.The investigation focuses on the effects of spacing ratio (/) m LD and wavy surface on the 3-D near wake flow patterns, the force and pressure coefficients and the vortex shedding frequency for the two tandem wavy cylinders. Flows around the two tandem circular cylinders are also obtained for comparison. the spacing ratio in the range of / = 1.5-5.5m LD, unlike two tandem circular cylinders, the wavy cylinders in the tandem arrangement do not have the wake interference behavior of three basic types.The vortex shedding behind the upstream wavy cylinder occurs at a further downstream position as compared with that of the upstream circular cylinder. This leads to the weakening of the effect of the vibration of the cylinders as well as a distinct drag reduction. The effects of the drag reducti on and the control of the vibration of the two wavy cylinders in tandem become more and more evident when / m L D 4.0, with a distinct vortex shedding in the upstream cylinder regime for the two circular cylinders in tandem.