Additional information:Use policyThe full-text may be used and/or reproduced, and given to third parties in any format or medium, without prior permission or charge, for personal research or study, educational, or not-for-prot purposes provided that:• a full bibliographic reference is made to the original source • a link is made to the metadata record in DRO • the full-text is not changed in any way The full-text must not be sold in any format or medium without the formal permission of the copyright holders.Please consult the full DRO policy for further details. Flow interaction between a streamwise oscillating cylinder and a downstream stationary cylinderReceived: date / Accepted: dateAbstract In this paper we present some experimental results about the physical effects of a cylinder's streamwise oscillation motion on a downstream one in a tandem arrangement. The upstream cylinder undergoes a controlled simple harmonic oscillation at amplitudes A/d = 0.2 ∼ 0.8, where d is the cylinder diameter, and the frequency ratio of f e /f s = 0 ∼ 3.0, where f e is the cylinder oscillation frequency and f s is the natural frequency of vortex shedding from a single stationary cylinder. Under these conditions, the vortex shedding is locked to the controlled oscillation motion. Flow visualization using the planar laser-induced fluorescence (LIF) and qualitative measurements using hot-wire anemometry (HWA) reveal three distinct flow regimes behind the downstream cylinder. For f e /f s > (f e /f s ) c , where (f e /f s ) c is a critical frequency ratio which depends on A/d and Reynolds number Re, a so called SA-mode occurs. The upstream oscillating cylinder generates binary vortices symmetrically arranged about the centreline, each containing a pair of counterrotating vortices, and the downstream cylinder sheds vortices alternately at 0.5f e . For 0.7 ∼ 1.0 < f e /f s < (f e /f s ) c a complex vortex street that consists of two outer rows of vortices generated by the oscillating cylin- der and two inner rows of vortices shed from the downstream stationary cylinder, which is referred to as AAmode. For 0.3 ∼ 0.6 < f e /f s < 0.8 ∼ 1.0, one single staggered vortex street (A-mode) is observed. It also is found that, when f e /f s is near unity, the streamwise interaction of the two cylinders gives rise to the most energetic wake in the corss-stream direction, in terms of its maximum width, and the wake is AA-mode like. The effects of other parameters such as the spacing between the two cylinders, Re and A/d on the flow pattern are also discussed in details. The observations are further compared to the stationary tandem cylinder cases.