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Compression Failure of Trabecular Tantalum Scaffolds
           Guangdong, China) at room temperature (25°C). Relative   Inc.,  Oberkochen,  Germany)  before  metallographic
           density was calculated by dividing the actual weight (W )   sample preparation.
                                                         1
           by the theoretical weight (W ) of the macrovolume using
                                   2
           a theoretical density (16.6 g/cm ) of pure Ta. The porosity   (2) Metallographic sample preparation
                                     2
           of scaffolds was obtained using the formula as follows:  Post-compressive  AM  trabecular  Ta  scaffolds  were
                                                               prepared  to metallographic  specimens  through the
                                  W                          vacuum pressure impregnation resin (VPIR) method .
                                                                                                            [28]
                  Porosity(%) = 1 −  1    ×100         (1)    Twenty  gram  of  acrylic  powder  (G90500,  Gaopin
                               
                               
                                  W 
                                                               Precision Instrument Co., Ltd., Kunshan, Jiangsu, China)
                                    2
               The microstructural  characteristics  of  AM-   and  40  ml  liquid  hardener  (G90400,  Gaopin  Precision
           fabricated porous Ta scaffolds were visualized using hot   Instrument Co., Ltd., Kunshan, Jiangsu, China) were
           field  emission  scanning  electron  microscopy  (FESEM)   mixed and stirred uniformly at room temperature (25°C).
           (MERLIN  Compact,  Carl  Zeiss  Inc.,  Oberkochen,   Metallographic inlay molds (φ20 mm × H20 mm) were
           Germany)  equipped  with  energy-dispersive  X-ray   used  to  prepare  metallographic  specimens.  Vacuum
           spectroscopy (EDS), which was used to ascertain  the   defoaming (SIE-MIX80, SIENOX Co., Ltd., Guangzhou,
           chemical compositions of the samples.               Guangdong, China)  was employed  to  exhaust  the  air
                                                               that remained in porous Ta scaffolds, making the resin
           2.3. Mechanical testing                             solution fully infiltrate into the pores of scaffolds. Then,

           To evaluate the mechanical properties of  AM-       the metallographic  specimens were placed  at room
           fabricated cylindrical trabecular Ta scaffolds (φ10 mm   temperature for 12 h to complete resin solidification. In
           × H10 mm), 6 samples (n = 6) from each group (65%,   addition, an uncompressed porous  Ta metallographic
           75%,  and  85%)  were  subjected  to  uniaxial  static   sample  was prepared  for  each  porosity  as the  control
           compression  testing  at  room  temperature  (25°C).   group.
           Compression tests were performed in accordance with
           ISO 13314:2011 (mechanical testing of metals-ductility   (3) Grinding and polishing
           testing-compression test for porous and cellular    Grinding and polishing of as-prepared metallographic
           metals) using mechanical testing machine (max. 5 kN,   specimens were conducted by a metallographic sample
           Instron 4301, Instron Company, Norwood, MA, USA)    grinding and polishing machine (YMP-2B, Metallurgical
           equipped with an extensometer (YSJ50/5-ZC, Suzhou   Equipment Co., Ltd., Shanghai, China) with a sandpaper
           Shenghui Precision Instrument Technology Co., Ltd.,   diameter  of  230  mm.  Metallographic  specimens  were
           Suzhou, Jiangsu, China). A constant deformation rate   ground using 100, 200, 400, 800, 1200, 1500, and 2000
           of 0.5 mm/min was applied during compression tests.   SiC papers and then polished by diamond suspensions with
           Each  specimen  was  compressed  to  50%  strain  to   sizes of 5, 2, and 0.5 μm. To achieve the same polished
           obtain  stress–strain  curves.  The  elastic  modulus  (E)   cross section, 3 metallographic specimens of each porosity
           as the gradient of the straight line was calculated from   were ground under an identical extent and direction.
           the linear deformation region at the beginning of the   The schematic of porous  Ta metallographic sample
           compressive stress–strain curve. The compressive 0.2%   preparation is presented in Figure 2. The morphological
           offset stress was identified from the stress–strain curve   characterizations of the metallographic specimens were
           as the yield strength (σ ).                         observed  by  electron  backscattered  diffraction  (EBSD,
                               y
           2.4. Experimental study of compressive behavior     Carl Zeiss Inc., Oberkochen, Germany).
           and material failure                                2.5. FEA
           (1) Static compression testing                      FEA was performed to simulate the mechanical behaviors

           To obtain the initial stages of trabecular Ta scaffolds after   of trabecular Ta scaffolds under quasi-static compressive
           collapse  under  static  compressive  loading,  10%,  15%,   loading  by  Abaqus/CAE  2020  (Dassault  Systemes
           and 20% strain were set for specimens with 65%, 75%,   Simulia Co., Johnston, RI, USA).  Considering the
           and 85% porosities, respectively. Two specimens of each   simulation efficiency and required accuracy, a 5 mm ×
           porosity (annealed  and unannealed) were prepared for   5 mm (diameter × height) model with the same porous
           compression tests with an identical strain. Compression   structure characteristics as the as-fabricated samples were
           tests were performed under the same equipment  and   applied in this simulation. Ten-node quadratic tetrahedron
           deformation  rate  as mechanical tests described  above.   (C3D10) with an element size of 0.08 mm was chosen to
           Post-compressive  microstructures of all  samples  were   mesh this FEA model, and material properties were set
           observed by hot FESEM (MERLIN Compact, Carl Zeiss   according to pure Ta, consisting of an elastic modulus of

           114                         International Journal of Bioprinting (2022)–Volume 8, Issue 1
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