2017
DOI: 10.1016/j.ijfatigue.2016.11.009
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Experimental study of the low-cycle fatigue life under multiaxial loading of aluminum alloy EN AW-2024-T3 at elevated temperatures

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Cited by 30 publications
(17 citation statements)
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“…Another important phenomenon [89][90][91][92][93][94] affecting capsule shells is the cyclic thermal loading during charging/discharging as well as stresses generated by the expanding PCM material. Although the repeated loads applied during solidification or melting of the PCM are below certain threshold, e.g., yield strength, after dozens of cycles microscopic cracks start to develop and when the critical size of the crack is reached, the structure fractures suddenly.…”
Section: Results and Analyses Of The Epcm Shellmentioning
confidence: 99%
“…Another important phenomenon [89][90][91][92][93][94] affecting capsule shells is the cyclic thermal loading during charging/discharging as well as stresses generated by the expanding PCM material. Although the repeated loads applied during solidification or melting of the PCM are below certain threshold, e.g., yield strength, after dozens of cycles microscopic cracks start to develop and when the critical size of the crack is reached, the structure fractures suddenly.…”
Section: Results and Analyses Of The Epcm Shellmentioning
confidence: 99%
“…Next, the proposed fatigue damage accumulation model was also verified for the case of multiaxial loads. The results of original experimental tests performed on the EN AW-2024T3 aerospace aluminum alloy were used for this purpose [5]. Figure 11 presents normalized evolutions of the damage state variable, plotted for load paths RS0 and RS90 at the analyzed temperature.…”
Section: Resultsmentioning
confidence: 99%
“…Figure 11 presents normalized evolutions of the damage state variable, plotted for load paths RS0 and RS90 at the analyzed temperature. A comparison between the results of experimental tests and of numerical simulations using the proposed SS2 approach (Equation (10)) and the SS1 semi-empirical model (Equation (2)) described in Reference [5] is given in Figure 12 and in Table 6. Next, the proposed fatigue damage accumulation model was also verified for the case of multiaxial loads.…”
Section: Resultsmentioning
confidence: 99%
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