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Tables of Contents for Life Assessment of Hot Section Gas Turbine Components
Chapter/Section Title
Page #
Page Count
Introduction
vii
Design Issues for Aeroengines
1
10
Lifing Strategies for High Temperature Fracture Critical Components
11
24
Life Management Issues for Operators
35
14
Microstructural Design of IN706-type Disc Materials for Improved Creep Crack Growth Resistance
49
12
Fatigue in Modern Nickel-Base Alloys for Gas Turbine Applications
61
22
Influence of Creep and Oxidation on the Elevated Temperature Crack Growth Behaviour of a Near-α Titanium Alloy
83
14
Effects of Grain and Precipitate Size Variation on Creep-Fatigue Behaviour of Udimet 720Li
97
12
Modelling of Creep Strain Behaviour of Udimet 720Li Wrought Superalloy
109
10
Characterisation of Damage Accumulation During the Creep Deformation of CMSX-4 at 1150°C
119
16
Coating Life Assessment
135
20
Combined Effects of Temperature Gradient and Oxidation on Thermal Barrier Coating Failure
155
18
Investigation of Microstructural Development of PtAl Diffusion Coatings
173
12
Diffusion Barriers for Gas Turbine Superalloy Blades
185
8
Thermomechanical Fatigue of Coated Superalloys
193
16
High Temperature Deformation and Crack Growth in γ-TiAl Base Intermetallic Materials
209
20
Application of Thermal Barrier Coatings on NiAl Intermetallic Material
229
8
Residual Life Assessment: Approaches, Techniques and Questions
237
12
Life Management System for Combustion Turbine Blades and Vanes
249
22
Predicting the Remnant Life of Corrosion Resistant Coatings
271
10
A Modelling Approach to Gas Turbine Blade Life Management
281
12
Stress Relaxation as a Basis for Blade Creep Life Assessment
293
18
Microstructural Evaluation of MCrAIY/Superalloy Interdiffusion Zones
311
16
The Development of a Process Model for the Weldability of Nickel-Base Superalloys for Gas Turbine Applications
327
12
Author Index
339
1
Subject Index
340