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Crystallographic fatigue crack growth in nimonic AP1
J.E. King
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Corresponding author for this work
Aston University
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Keyphrases
Aluminum Alloy
16%
Crack Propagation
16%
Crystallization Crack
16%
Fatigue Crack Growth
100%
High Stress
16%
Left Braces
100%
Low Stress
16%
Near-threshold
16%
Nickel-based Superalloy
16%
Nimonic
100%
Room Temperature
16%
Slip Plane
16%
Stress Intensity
33%
Work Crack
16%
Engineering
Crack Growth
50%
Crack Propagation
50%
Fatigue Crack Growth
100%
Flat Surface
100%
Room Temperature
50%
Slip Plane
50%
Stress Intensity
100%
Medicine and Dentistry
Aluminum
100%
Base
100%