Skip to main content
Journal of Materials Science: Materials in Engineering
Figure 8 | International Journal of Mechanical and Materials Engineering

Figure 8

From: High-cycle fatigue investigations of notched Glare under different stress ratio's in various environments

Figure 8

Comparative plots between plain aluminum alloy specimens and case I laminate.a) Crack length vs. number of cycles in laminate (Series 1) and plain specimens b) Crack length vs. crack growth rate in laminate (Series 1) and plain specimens c) Cyclic induced stress intensity parameter vs. crack growth rate in laminate (Series 1) and plain specimens d) Cyclic applied stress intensity parameter vs. crack growth rate in laminate (Series 1) and plain specimens.

Back to article page