1972
DOI: 10.1016/0025-5416(72)90038-9
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Effect of stress cycle asymmetry on fatigue crack growth

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Cited by 214 publications
(50 citation statements)
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“…Figure 2 shows the variation of the values of AKg with R for each material obtained when no growth was detected after lo7 cycles. Using the relation put forward by Klesnil and Lukas [7] and ignoring stress history effects, their equation can be reduced to:…”
Section: Air Testsmentioning
confidence: 99%
“…Figure 2 shows the variation of the values of AKg with R for each material obtained when no growth was detected after lo7 cycles. Using the relation put forward by Klesnil and Lukas [7] and ignoring stress history effects, their equation can be reduced to:…”
Section: Air Testsmentioning
confidence: 99%
“…The value of K , can be regarded as being the plane strain fracture toughness K,,, a material property, the calculation of which is well defined and which is independent of load, specimen configuration, etc. However, the same is not true of A K T , which has been shown to vary according to loading conditions [6,7]. Thus the value of AKT is not simply defined and needs to be determined for each type of fatigue loading considered.…”
mentioning
confidence: 99%
“…For example, the linear fit proposed by Barson (1974), Eq. (5), and the power fit proposed by Klesnil and Lukáš (1972), Eq. (6):…”
Section: Procedures and Data Elaborationmentioning
confidence: 99%