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06998cam a2200997 i 4500 |
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946949070 |
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OCoLC |
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20240223121953.0 |
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|a com.springer.onix.9789811009198
|b Springer Nature
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|a Sadowski, Tomasz,
|d 1954-
|1 https://id.oclc.org/worldcat/entity/E39PCjKkGCXdMfb7TPBbJGP6yq,
|e author.
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| 245 |
1 |
0 |
|a Loadings in thermal barrier coatings of jet engine turbine blades :
|b an experimental research and numerical modeling /
|c Tomasz Sadowski, Przemysław Golewski.
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| 264 |
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1 |
|a Singapore :
|b Springer,
|c 2016.
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| 300 |
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|a 1 online resource (viii, 107 pages) :
|b illustrations (some color).
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| 336 |
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|a text
|b txt
|2 rdacontent.
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| 337 |
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|a computer
|b c
|2 rdamedia.
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| 338 |
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|a online resource
|b cr
|2 rdacarrier.
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| 347 |
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|a text file.
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| 347 |
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|b PDF.
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| 490 |
1 |
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|a SpringerBriefs in applied sciences and technology, Computational mechanics,
|x 2191-530X.
|
| 504 |
|
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|a Includes bibliographical references.
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| 588 |
0 |
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|a Online resource; title from PDF title page (SpringerLink, viewed April 19, 2016).
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| 520 |
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|a 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.
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| 505 |
0 |
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|a 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.
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| 505 |
8 |
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|a 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.
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8 |
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|a 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.
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| 505 |
8 |
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|a 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.
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| 546 |
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|a English.
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| 650 |
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|a Thermal barrier coatings.
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| 650 |
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|a Aircraft gas-turbines
|x Blades
|x Materials.
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| 650 |
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6 |
|a Revêtements de barrières thermiques.
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| 650 |
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6 |
|a Avions
|x Turbines à gaz
|x Aubes
|x Matériaux.
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| 650 |
|
7 |
|a TECHNOLOGY & ENGINEERING
|x Chemical & Biochemical.
|2 bisacsh.
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| 650 |
|
7 |
|a Thermal barrier coatings.
|2 fast.
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| 700 |
1 |
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|a Golewski, Przemysław,
|e author.
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| 710 |
2 |
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|a SpringerLink (Online service)
|
| 776 |
0 |
8 |
|i Printed edition:
|z 9789811009181.
|
| 830 |
|
0 |
|a SpringerBriefs in applied sciences and technology.
|p Computational mechanics.
|x 2191-530X.
|
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