Springer Science+Business Media Singapore Pte Ltd., 2016. – 110 p. – ISBN10: 981100918X
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.
TopicsContinuum Mechanics and Mechanics of Materials
Characterization and Evaluation of Materials
Mathematical Modeling and Industrial Mathematics
Machinery and Machine Elements
Protective Thermal Barrier Coatings
Thermal Loads
Mechanical Loads
Environmental Loads
State of Arts in Experimental Testing of TBCs Systems—Literature Analysis
Proposed Experimental Investigations of TBCs Systems
Numerical Analysis of Cracks Propagation Process in Turbine Blades TBCs Systems Under Thermo-Mechanical Loading Based on Experimental Results