... compressor blade section across the same range of operating conditions. The results show that large laminar separation bubbles exist on both blade surfaces. As Reynolds number increases, these separation bubbles shorten in length and reduce in thickness. Correspondingly, the downstream wake narrows, although...

... interactions laminar separation bubble surface hot-film transition boundary layer development measurement techniques turbine measurement advancements The interaction of shock waves with boundary layers is subject of numerous research projects since more than half a century [ 1 ]. A lot...