Loadings in thermal barrier coatings of jet engine turbine blades : an experimental research and numerical modeling /: an experimental research and numerical modeling. (2016)

• Record Type: Book
• Further Information: Note: Tomasz Sadowski, Przemysław Golewski.
• Authors: Sadowski, Tomasz, 1954-; Golewski, Przemysław
• Contents: Preface; Acknowledgement; Contents; 1 Introduction; 2 Protective Thermal Barrier Coatings; 2.1 Structure of TBCs; 2.2 Development and Application of New Coating Materials; 2.3 Conclusions; References; 3 Thermal Loads; 3.1 Numerical Methods-Application of Finite Elements Method (FEM) [1, 2]; 3.2 Deformation and Stress in Structural Elements, Caused by Thermal Loads [1, 2]; 3.3 Numerical Analysis of Temperature Fields in Critical Elements of Turbo-Engines by CFD (Computational Fluid Dynamics) with Application of FLUENT Program; 3.4 Conclusions; References; 4 Mechanical Loads. 4.1 Preparation of Model for Simulation4.2 Analysis of Results; 4.3 Blade Vibrations Resonance; 4.4 Conclusions; Reference; 5 Environmental Loads; 5.1 Corrosion; 5.2 Erosion; 5.3 Thermally Growth Oxide (TGO) Layer Growth; 5.4 Author's Own Tests of Moving Blade Surface, Including Chemical Analysis; 5.5 Conclusions; References; 6 State of Arts in Experimental Testing of TBCs Systems-Literature Analysis; 6.1 Review and Analysis of Currently Utilised Tests; 6.2 Conclusions; References; 7 Proposed Experimental Investigations of TBCs Systems; 7.1 Sample Ageing. 7.2 Uniaxial Stretching of Dumbbell Samples with TBC Layers-Author's Own Tests7.2.1 First Batch of Samples Not Subjected to Ageing; 7.2.2 Second Batch of Samples Subjected to Ageing; 7.3 3-Point Bending of Beam Samples with TBC Layers-Author's Own Tests; 7.4 Conclusions; 8 Numerical Analysis of Cracks Propagation Process in Turbine Blades TBCs Systems Under Thermo-Mechanical Loading Based on Experimental Results; 8.1 Formulation of FEM Approach and Brittle Damage of the TBCs System; 8.1.1 Brittle Damage Model; 8.1.2 Cohesive Degradation Model; 8.1.3 Simulation Results. 8.2 Application of Submodeling Technique and X-FEM Methods for Detailed Analysis of Cracking Process in Turbine Blades TBCs8.2.1 Submodeling; 8.2.2 X-FEM Method Basics; 8.2.3 Preparation of Model for Simulation; 8.3 Analysis of Results; 8.4 Conclusions; References; 9 Summary.
• Publisher Details: Singapore : Springer
• Publication Date: 2016
• Extent: 1 online resource (viii, 107 pages), illustrations (some color)
• Subjects: 667/.9; Thermal barrier coatings; Aircraft gas-turbines -- Blades -- Materials; TECHNOLOGY & ENGINEERING -- Chemical & Biochemical; Thermal barrier coatings; Engineering; Continuum Mechanics and Mechanics of Materials; Characterization and Evaluation of Materials; Mathematical Modeling and Industrial Mathematics; Machinery and Machine Elements; Electronic books
• Languages: English
• ISBNs: 9789811009198; 9811009198; 9789811009181
• Related ISBNs: 981100918X; 9789811009181
• Notes: Note: Includes bibliographical references.; Note: Online resource; title from PDF title page (SpringerLink, viewed April 19, 2016).
• Access Rights: Legal Deposit; Only available on premises controlled by the deposit library and to one user at any one time; The Legal Deposit Libraries (Non-Print Works) Regulations (UK).
• Access Usage: Restricted: Printing from this resource is governed by The Legal Deposit Libraries (Non-Print Works) Regulations (UK) and UK copyright law currently in force.