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. 2021 May 14;14(10):2564. doi: 10.3390/ma14102564

Figure 4.

Figure 4

(a) Fatigue properties (S-N curves) of different AA1050/AA5754 N2 LMC architectures and constituent monolithic materials. Data partly adapted from [15,32,46]. The percentile of fatigue crack propagation on total fatigue life is indicated in the respective LCF regimes; (b) schematic illustration of the LMC architectures; (c) determination of the onset of fatigue crack propagation in the LCF regime for a monolithic and LMC sample using a 0.1 Hz resonance frequency drop criterion.