Fig. 14From: Static fracture and modal analysis simulation of a gas turbine compressor blade and bladed disk systemClose-up view of the extreme deformed shapes corresponding to the first bending mode (Mode 1) localized around blade with crack depth \(=\) 4Â mm. a Extreme mode shape. b Opposite extreme mode shape. c Zoom around crack in extreme mode shape. d Zoom around crack in opposite extreme mode shapeBack to article page