To investigate the effects of the inclined ribs on internal flow structure in film hole and the film cooling performance on outer surface, experimental and numerical studies are conducted on the effects of rib orientation angle on film cooling of compound angle holes. Three coolant channel cases, including two ribbed cross-flow channels (135 degrees and 45 degrees inclined ribs) and the plenum case, are studied for three blowing ratios. The 2D contours of film cooling effectiveness and heat transfer coefficient are measured by transient liquid crystal measurement technique. The steady BANS simulations with realizable k-epsilon turbulence model and enhanced wall treatment are performed. The results show that the lateral spread of the coolant jet on the surface is paramount influenced by the rib orientation angle. The lateral spread of the 45 degrees rib case is obviously larger than that of the 135 degrees rib case for lower blowing ratios. For the blowing ratio of 1.0, the area-averaged cooling effectiveness for the 135 and 45 degrees rib angles is higher by a factor of 38% and 107%, respectively, compared to the plenum case. With the increase of blowing ratio, the film coverage difference becomes smaller between different rib orientation cases. The 45 degrees rib case also produces a higher heat transfer coefficient, which is higher than the 135 degrees rib case by 3.4-8.7% within the studied blowing ratio range. The discharge coefficient of the 45 degrees rib case is the lowest among the three cases. The helical motion of coolant flow is observed in the hole of the 45 degrees rib case. The jet divides into two parts after ejecting out of the hole due to this motion, which results in the strong velocity separation and loss. For the 135 degrees rib case, the vortex in the upper half region of the secondary-flow channel rotates in the same direction with the hole inclination direction, which leads to the straight streamlines and thus results in lower loss and higher discharge coefficient. (C) 2018 Elsevier Ltd. All rights reserved.