This book discusses complex loadings of turbine blades and protective layer Thermal Barrier Coating (TBC), under real working airplane jet conditions. They obey both multi-axial mechanical loading and sudden temperature variation during starting and landing of the airplanes. In particular, two types of blades are analyzed: stationary and rotating, which are widely applied in turbine engines produced by airplane factories.
TBC Turbine blade Submodelling X-FEM EDS Aramis system Acoustic emission
Authors and affiliations
1.Department of Solid MechanicsLublin University of TechnologyLublinPoland
2.Department of Solid MechanicsLublin University of TechnologyLublinPoland