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Materials Science in Additive Manufacturing                  Energy absorption of Moore’s thin-walled structures




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            Table 3. Specific energy absorption for the 4  order   for 4  order structures. However, the SEA in LD1 was more
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            structures subjected to quasi‑static compressive loadings  sensitive to increment in relative density compared to LD2.
                                                               By comparing the values in Table 3 and Figure 11, it could
             SEA (J/kg)            4  order structure          be extrapolated that SEA decreases with the increase in
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                         Loading direction 1  Loading direction 2  fractal hierarchy after the 2  order. The compliance feature
                                                                                    nd
            rd=20%            67.05              64.77         and snap-in instability are more pronounced in higher
            rd=30%            321.94             211.88        orders, and the strength of the structures is sacrificed.
            rd=40%            491.68             339.08        Therefore, the energy absorption capacities are reduced for
                                                                                               nd
            rd: relative density                               high order structures (higher than the 2  order).
                                                               4. Conclusions
            3.5. Parametric study
            A parametric study using FE simulation was conducted   This paper presents a series of thin-walled structures
            on 4   order structures with different relative densities   inspired by Moore space-filling curves. Nine designs,
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            to further explore the influences of fractal hierarchy and   featuring three hierarchies with three relative densities, that
            relative density on structural responses. To compare   is, 20%, 30%, and 40%, were proposed and investigated.
            the responses of the 4   order structures with the 1 ,   The FFF 3D printing technology was used to manufacture
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                                                         st
            2 , and 3   order structures, the effective stress-strain   the samples with carbon fiber-reinforced nylon. Both
                    rd
             nd
            curves of the 3  order structures were used as references   quasi-static and loading-unloading compression tests were
                        rd
            (Figure 13A and B). As revealed in Figure 13A and B (left   conducted to obtain and analyze the mechanical responses
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            panels), the 4   order structures yielded more compliant   and energy absorption capacity of the proposed structures.
            behaviors than the 3  order structures at any given relative   Simulations were also performed to further elaborate the
                            rd
            density in both LD1 and LD2. The increase by one fractal   mechanical behaviors that were not observed from the
            order led to quadruple complexity and meandering features   experiment, that is, stress distribution. Herein,  several
            in the cross-sectional configuration. The large number of   conclusions were drawn.
            curved segments gave rise to more snap-in instability and   (i)  The space-filling feature of Moore curves offered
            structural compliance, which were also manifested in more   great compliance to the thin-walled structures. All
            serrated stress-strain curves of the 4  order structures.  the fractal structures exhibited high level of flexibility,
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              Figure 13A and B (right panels) shows clearer effective   which could provide great potential for energy
            stress-strain curves of the 4   order structures, while   absorbing device with large strain endurance before
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            Figure  13C  and  D displays the structural deformations   failure. Fractal hierarchy was positively related to
            of the 4   order structures under compression from    compliance, while relative density was the opposite.
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            LD1 (rd = 20%) and LD2 (rd = 30%), respectively. With   (ii)  The meandering pattern of Moore space-filling curves
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            the increase in relative density, the 4   order structure   and the smooth geometry design enabled the snap-in
            experienced higher stress in both in-plane directions due   of  thin-walled  structures.  A  certain  degree  of  such
            to its thicker wall-thickness. The drastic stress drops were   instability reduced the stress within the structures,
            created by the multiple simultaneous snap-ins (see 20%   enhancing  the  energy  absorption  capacity.  The
                                                                   nd
                                                                                                        rd
                                                                                                     st
            strain in Figure 13C and D). A plateau phase (Figure 13B   2   order structures outperformed the 1 , 3 , and
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            [right panel]) in the effective stress-strain curves at a   4  order structures in absorbing energy.
            strain of 40% after the stress jump could be observed for   (iii) During  quasi-static  compression  test,  the  SEA
            all 4  order structures in LD2. This could be explained by   was relatively higher when subjected to LD2 than
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            the structural deformation in Figure 13D. After the 30%   when subjected to LD1 due to the cross-sectional
            strain, both sides of the structure expanded outward in   configuration and snap-in behavior.
                                                                                        nd
            a transverse direction. The snap-ins along the side edges   (iv)  In cyclic loading tests, the 2  order structure exhibited
            eventually unlocked and slid further outward, resulting   better resilience. Smaller energy dissipation ratio and
            in a long plateau phase. However, this was not observed   less residual strain indicated the promising ability
            in LD1 as only flat surface contacts, without snap-ins,   of the 2   order structure to resist deformation and
                                                                         nd
            occurred along the longitudinal edges (Figure 13C).   damage from external loadings.
              Table 3 summarizes the corresponding SEA for the   Overall, the proposed designs inspired by Moore space-
            4   order  structures  under  different  loading  directions.   filling curves in the present study open a new avenue for
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            Consistent with the results obtained from the first three   further research into the field of lightweight structures
            orders, SEA has a positive relationship with relative density   for energy absorption. The combination of thin-walled


            Volume 2 Issue 1 (2023)                         13                       https://doi.org/10.36922/msam.53
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