“…Following the early thermal investigations of cyclone cooling in swirl tubes [ (Glezer et al, 1996), (Hedlund and Ligrani, 2000)], more sophisticated experimental studies were done to analyze the internal flow structure in swirl tubes (Biegger et al, 2013) with different channel outlet geometries (Grundmann et al, 2012) and duct bends [ (Wassermann et al, 2013), (Bruschewski et al, 2020), (Wang et al, 2021)]. Numerical studies were carried out to understand the swirling flow in detail [ (Biegger et al, 2015), (Seibold and Weigand, 2021)], but the investigated geometries are still too simplified compared to the geometry of a real turbine blade. The effect of the swirling flow on the film cooling performance was investigated experimentally with the result that the orientation of the film cooling holes with respect to the swirl influences the discharge through the holes and thereby the film cooling effectiveness (Lerch et al, 2012).…”