“…Due to its high potential in enhancing local heat transfer, jet impingement has been widely used in turbine thermal load components, especially for the highest heat load portionthe blade leading edge, which directly suffers hot gas from combustor (Kwak and Han, 2002). Many significant works spent much efforts on the effects of jet Reynolds number, jet nozzle configuration, jet-to-target spacing, target arrangement and jet inclination angle on single jet impinging onto a confined or an unconfined concave or convex surface (Yang et al, 1999;Rahman et al, 2010;Qiu et al, 2019;Cornaro et al, 1999;Luo et al, 2016;Lee et al, 2007;Yang and Hwang, 2004).…”