The effect of N "SUB 2" and CO "SUB 2" environments on the fatigue failure of MAR-M200+Hf superalloy at 975 degreesC

Keyphrases

• Al-Ti 33%
• Alloying Elements 33%
• Auger Electron Spectroscopy 33%
• Catalytic Decomposition 33%
• Chemical Interaction 66%
• Crack Growth Characteristics 33%
• Crack Initiation 33%
• Crack Propagation 33%
• Crack Tip 33%
• Creep 33%
• Dendritic Grain 33%
• Failure Mechanism 33%
• Fatigue Crack Growth Rate 33%
• Fatigue Failure 100%
• Fatigue Mechanism 33%
• Gaseous Environment 33%
• High Temperature Low Cycle Fatigue 100%
• Interdendritic Region 33%
• Internal Nitridation 33%
• Internal Oxidation 33%
• Loading Conditions 33%
• Low Cycle Fatigue 33%
• Low-cycle Fatigue Crack Growth 66%
• Microsegregation 33%
• Nickel-based Superalloy 33%
• Partitioning Method 33%
• Plastic Compressibility 33%
• Propagating Crack 33%
• Scanning Electron Microscopy 33%
• Strain Range Partitioning 33%
• Superalloy 100%
• Tension-compression 33%
• Transgranular 33%
• X Ray Diffraction 33%

Engineering

• Alloying Element 33%
• Crack Growth Behavior 33%
• Crack Initiation 33%
• Crack Propagation 33%
• Crack Tip 33%
• Creep 33%
• Failure Mechanism 33%
• Fatigue Crack Growth 66%
• Fatigue Failure 100%
• Internals 33%
• Loading Condition 33%
• Low Cycle Fatigue 100%
• Microsegregation 33%
• Propagating Crack 33%
• Ray Diffraction 33%

Material Science

• Alloying 33%
• Auger Electron Spectroscopy 33%
• Crack Initiation 33%
• Crack Propagation 33%
• Crack Tip 33%
• Creep 33%
• Fatigue Crack Growth 66%
• Low-Cycle Fatigue 100%
• Nickel-Based Superalloys 33%
• Nitriding 33%
• Oxidation Reaction 33%
• Scanning Electron Microscopy 33%
• Superalloys 100%
• X-Ray Diffraction 33%