“…Cornaro et al (1999) found that a cylinder-jet diameter ratio as low as approximately 2.5 could produce relatively stable and well-formed vortex structures along the impingement surfaces, though it has to be highlighted that their jet Reynolds number was quite a bit higher at Re = 6000. Note also that Shim et al (2014) and Singh et al (2013) demonstrated that a wake region exists behind the circular cylinder during jet impingement. Therefore, using cylinder-jet diameter ratio of D/d = 2 will allow the present study to focus upon both the resultant vortex structures and their behaviour, as well as on the wake region at the cylinder lee side.…”