Mechanics of Fatigue Crack Closure 1988
DOI: 10.1520/stp27233s
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Influence of Fatigue Crack Wake Length and State of Stress on Crack Closure

Abstract: The location of crack closure with respect to crack wake and specimen thickness under different loading conditions was determined. The rate of increase of K_. in the crack wake was found to be significantly higher for plasticity induced closure 1n comparison to roughness induced closure. enRoughness induced closure was uniform throughout the thickness of the specimen en en ™ while plasticity induced closure levels were 50 percent higher in the near uu surface region than in the mid-thickness. The influence of … Show more

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Cited by 2 publications
(5 citation statements)
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“…The concept presented in Fig. 6 seems to be supported by an experimental research on the effect of fatigue crack wake removal and specimen surface removal on crack closure behaviour in Al alloy CT specimens subjected to CA loading 77 . In the latter study, incremental wake removal did not affect K op at higher Δ K levels even if the remaining wake length was only 0.33 mm, whilst under a near‐threshold Δ K a gradual decrease in K op started already at the remaining wake length of 4 mm, as schematically shown in Fig.…”
Section: Effect Of Loading Variablesmentioning
confidence: 64%
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“…The concept presented in Fig. 6 seems to be supported by an experimental research on the effect of fatigue crack wake removal and specimen surface removal on crack closure behaviour in Al alloy CT specimens subjected to CA loading 77 . In the latter study, incremental wake removal did not affect K op at higher Δ K levels even if the remaining wake length was only 0.33 mm, whilst under a near‐threshold Δ K a gradual decrease in K op started already at the remaining wake length of 4 mm, as schematically shown in Fig.…”
Section: Effect Of Loading Variablesmentioning
confidence: 64%
“…In this type of experiment, fatiguing a cracked specimen is interrupted and material from the specimen outer surfaces is incrementally removed, while closure is measured at each new thickness. Provided that Δ K is not near‐threshold, surface removal tests 77 , 86 reveal the trend seen at high Δ K in Fig. 7(b), indicating that after removing the ‘plane stress’ regions, the PICC mechanism is weakened, but still active.…”
Section: Crack Closure In Plane Strain Conditionsmentioning
confidence: 91%
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