“…However, experiments show that under-loads do not create retardation effect as the overloads do and they can even cause a slight acceleration of the fatigue crack growth [57].…”
Section: Constant Amplitude Loading History Interrupted By a Single Omentioning
confidence: 97%
“…Russ [57] with the aim to investigate the load-interaction effect in the case of constant amplitude loading with repeatable single underloads. The fatigue crack growth was studied in compact tension specimens (Figure 6-2) made of Ti-17 titanium alloy subjected to special type of loading spectra shown in Figure 6-3.…”
Section: Fatigue Crack Growth In the Ti-17 Titanium Alloy Under Constmentioning
confidence: 99%
“…The fatigue crack growth was studied in compact tension specimens (Figure 6-2) made of Ti-17 titanium alloy subjected to special type of loading spectra shown in Figure 6-3. The stress intensity factor expression used in the study [57] was: …”
Section: Fatigue Crack Growth In the Ti-17 Titanium Alloy Under Constmentioning
confidence: 99%
“…All relevant data concerning analysed loading spectra were borrowed from reference [57] and they are also shown in Table 7-1. These include the maximum applied load, the ratio between maximum and minimum applied load of the baseline loading cycles and the underloading levels, and the number of spacing cycles between underloads.…”
Section: Fatigue Crack Growth In the Ti-17 Titanium Alloy Under Constmentioning
confidence: 99%
“…Cyclic stress-strain experimental data was also borrowed from reference [57]. The plastic strain vs. stress amplitude data points were extracted from the experimental total strain vs. stress data according to the standard procedure given in reference [54].…”
Section: Fatigue Crack Growth In the Ti-17 Titanium Alloy Under Constmentioning
“…However, experiments show that under-loads do not create retardation effect as the overloads do and they can even cause a slight acceleration of the fatigue crack growth [57].…”
Section: Constant Amplitude Loading History Interrupted By a Single Omentioning
confidence: 97%
“…Russ [57] with the aim to investigate the load-interaction effect in the case of constant amplitude loading with repeatable single underloads. The fatigue crack growth was studied in compact tension specimens (Figure 6-2) made of Ti-17 titanium alloy subjected to special type of loading spectra shown in Figure 6-3.…”
Section: Fatigue Crack Growth In the Ti-17 Titanium Alloy Under Constmentioning
confidence: 99%
“…The fatigue crack growth was studied in compact tension specimens (Figure 6-2) made of Ti-17 titanium alloy subjected to special type of loading spectra shown in Figure 6-3. The stress intensity factor expression used in the study [57] was: …”
Section: Fatigue Crack Growth In the Ti-17 Titanium Alloy Under Constmentioning
confidence: 99%
“…All relevant data concerning analysed loading spectra were borrowed from reference [57] and they are also shown in Table 7-1. These include the maximum applied load, the ratio between maximum and minimum applied load of the baseline loading cycles and the underloading levels, and the number of spacing cycles between underloads.…”
Section: Fatigue Crack Growth In the Ti-17 Titanium Alloy Under Constmentioning
confidence: 99%
“…Cyclic stress-strain experimental data was also borrowed from reference [57]. The plastic strain vs. stress amplitude data points were extracted from the experimental total strain vs. stress data according to the standard procedure given in reference [54].…”
Section: Fatigue Crack Growth In the Ti-17 Titanium Alloy Under Constmentioning
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