Fig. 6From: Static fracture and modal analysis simulation of a gas turbine compressor blade and bladed disk system a Comparison of Mode I, K\(_{\mathrm {I}}\) crack depth \(=\) 4Â mm, rotational velocity\(\,=\,\) 500Â rad/s. b Comparison of Mode II, K\(_{\mathrm {II}}\), crack depth \(=\) 4Â mm, rotational velocity\(\,=\,\) 500Â rad/s. c Comparison of Mode III, K\(_{\mathrm {III}}\), crack depth \(=\) 4Â mm, rotational velocity\(\,=\,\)500Â rad/sBack to article page