A Numerical Study on 3D Printed Cementitious Composites Mixes Subjected to Axial Compression
Abstract
:1. Introduction
2. Materials and Method
2.1. Fabrication and Testing
2.2. Performance Evaluation and Prediction by Modeling
2.2.1. Abaqus Concrete Smeared Cracking (CSC)
2.2.2. Maekawa–Fukuura Concrete Model (MFC)
2.2.3. Concrete Damaged Plasticity (CDP)
3. Results and Discussion
3.1. Compressive Performance
3.2. Numerical Modeling of the Cubes, Result Comparison and Validation
3.3. Modulation of FGC by Multilayering Approach Using CDP
3.4. Influence of Layer Volume
3.5. Influence of Layer Positions and Volume Reversal
3.6. Beyond a Two-Layer Configuration
4. Conceptual Applications
5. Conclusions
- The addition of glass fiber to concrete can improve the strain performance as multi-strength peaks and fairly extended strains. However, the addition of glass fiber to 3D printed concrete will influence printability and reduce the mechanical performance of the resulting printed concrete by the unavoidable imperfection of surface and internal voids.
- The addition of microsilica to concrete has the effect of a stretched-out post-failure regime. In other words, it considerably reduces the brittle failure of concrete by sustaining a large strain at maximum load. However, in 3d printing, microsilica can result in a highly cohesive mix, lacking adequate followability, thus yielding a highly stratified sample after printing resulting in print imperfections such as bulking or necking.
- For a two-layer configuration, the difference in the respective material strengths greatly influences the role of position and material volume. In other words, when the difference in material strength is high (Case 1, Case 2, Case 4, and Case 5), the stress–strain plot flips with position interchange, as shown in Cases 1 and 4 in Figure 4c,f. However, when the difference in strength is low, the position’s role is minimal, and layer volume governs the performance.
- When the stress–strain performances of the combined materials are similar, the resulting stress–strain plot amplifies the weaknesses and strengths of the source materials.
- The stress–strain behavior of the outer layer of concrete sample influences to a great extent the post-failure performance of the sample. Thus, in multilayering of concrete, the post-failure performance objective should influence the choice of materials regarding positioning. In addition, the peak strength should guide decision-making regarding volumetric ratios.
- A three-layer configuration model is influenced by volume if two of the three layers are allotted the same material. Furthermore, layer position has minimal to zero influence on the concrete models’ performance, provided each layer is allotted a different material and has equal volume.
Author Contributions
Funding
Data Availability Statement
Conflicts of Interest
Appendix A
Configuration | Volume (%) | Position | Width W (mm) | Length L (mm) | Height H (mm) | Thickness t (mm) |
---|---|---|---|---|---|---|
Two-layer | 25 | Inner | 50.00 | 50.00 | 100.00 | - |
75 | Outer | 100.00 | 100.00 | 100.00 | 25 | |
50 | Inner | 70.72 | 70.72 | 100.00 | - | |
50 | Outer | 100.00 | 100.00 | 100.00 | 14.64 | |
75 | Inner | 86.60 | 86.60 | 100.00 | - | |
25 | Outer | 100.00 | 100.00 | 100.00 | 6.7 | |
Three-layer | 33 | Inner | 57.73 | 57.73 | 100.00 | - |
33 | Middle | 81.65 | 81.65 | 100.00 | 11.95 | |
33 | Outer | 100.00 | 100.00 | 100.00 | 9.175 |
Appendix A.1. Compressive Stress–Strain Modeling
Appendix A.2. Tensile Stress–Strain Modeling
Appendix A.3. Boundary Conditions, Solvers, Loading Rate and Input Data
Compression | Tension | ||||||
---|---|---|---|---|---|---|---|
Yield Stress (N/mm2) | Inelastic Strain | Damage Parameters | Direct Strain | Yield Stress (N/mm2) | Fracture Energy (N.mm/mm2) | Damage Parameters | Displacement Rate |
27.4663 # | 0 # | 0 | 0.00095 | 3.531510255 | 0.1418483 | 0 | 0 |
40.0668 * | 6.949 × 10−5 * | 0 | 0.0014 * | 0.99 | 1 | ||
33.1797 | 0.00044819 | 0.1718 | 0.00155 | ||||
23.4759 | 0.00084542 | 0.4140 | 0.001625 | ||||
20.8940 | 0.00105616 | 0.4785 | 0.00175 | ||||
17.2352 | 0.00142766 | 0.5698 | 0.002 | ||||
10.1460 | 0.00196307 | 0.7467 | 0.0023 |
Compression | Tension | ||||||
---|---|---|---|---|---|---|---|
Yield Stress (N/mm2) | Inelastic Strain | Damage Parameters | Direct Strain | Yield Stress (N/mm2) | Fracture Energy (N.mm/mm2) | Damage Parameters | Displacement Rate |
15 # | 0 # | 0 | 0.0019 | 3.028683453 | 0.124446573 | 0 | 0 |
19.36424 * | 7.947 × 10−5 * | 0 | 0.0025 * | 0.99 | 1 | ||
11.07944 | 0.0016150 | 0.427840 | 0.003 | ||||
11.49108 | 0.00206361 | 0.406582 | 0.0035 | ||||
11.95366 | 0.00250579 | 0.382694 | 0.004 | ||||
7.5821 | 0.00355223 | 0.608448 | 0.0045 |
Compression | Tension | ||||||
---|---|---|---|---|---|---|---|
Yield Stress (N/mm2) | Inelastic Strain | Damage Parameters | Direct Strain | Yield Stress (N/mm2) | Fracture Energy (N.mm/mm2) | Damage Parameters | Displacement Rate |
12.4455 # | 0 # | 0 | 0.0019 | 1.7672209 | 0.117664076 | 0 | 0 |
16.47673 * | 4.618 × 10−5 * | 0 | 0.0024* | 0.99 | 1 | ||
14.96941 | 0.0007615 | 0.0914817 | 0.0029 | ||||
15.84147 | 0.0011369 | 0.0385549 | 0.0034 | ||||
14.18350 | 0.0018737 | 0.1391801 | 0.0039 | ||||
12.32112 | 0.002639 | 0.2522110 | 0.0044 | ||||
12.18422 | 0.0031593 | 0.2605198 | 0.0049 | ||||
11.529645 | 0.0037529 | 0.3002470 | 0.0054 |
Dilation Angle (°) | Eccentricity | fB0/fc0 | K | Viscosity Parameter | Density (t/mm3) | Young’s Modulus (N/mm2) | Poisson’s Ratio | ||
---|---|---|---|---|---|---|---|---|---|
35 | 0.1 | 1.16 | 0.67 | 0.007985 | 1.81 × 10−9 | 30,000 (C) | 8000 (GFC-1) | 7000 (MC-2) | 0.22 |
Appendix A.4. Stress Contributions and Effect of Interlayer Boundary Condition
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Constituent | SiO2 | Fe2O3 | AL2O3 | CaO + MgO | C | K2O + Na2O | |
---|---|---|---|---|---|---|---|
Weight percentage (%) | >88 | <1.0 | <1.0 | <0.7 | <1.5 | <1.5 | |
Property | Loss on Ignition | Moisture | PH value (pH) | Specific surface area (m2/kg) | Specific gravity | ||
Value | <3% | <2% | 4.5–8.5 | 15 | 2.3 |
Material | Length (mm) | Filament Diameter (mm) | Tensile Strength (MPa) | Elastic Modulus (MPa) | Density |
---|---|---|---|---|---|
Glass fiber | 3–6 | 0.5 | 1500–1700 | 72,000 | 2500 |
Category | Tag | Quarry Dust | OPC | Microsilica | Glass Fiber (% vol.) | SRI |
---|---|---|---|---|---|---|
Control (C) | Control | 900 | 600 | 80 | - | 0.94 |
Glass Fiber Concrete (GFC) | GFC-1 | 835 | 600 | 160 | 1.0 | 0.98 |
GFC-2 | 835 | 600 | 160 | 1.5 | 0.96 | |
GFC-3 | 835 | 600 | 160 | 2.0 | 0.94 | |
Microsilica Concrete (MC) | 16%MC-1 | 846 | 600 | 144 | 0.5 | 0.97 |
23%MC-2 | 792 | 600 | 207 | 0.5 | 0.96 | |
30%MC-3 | 739 | 600 | 270 | 0.5 | 0.96 |
Model Type | Post-Failure Stiffness | Yield Function | Flow Rule | Crack Detection | Damage Recovery (Loading and Unloading) | |
---|---|---|---|---|---|---|
CSC [50] | Continuum, smeared cracking. Cracks are fixed and limited to one per integration point | Damaged-elasticity, strain hardening, and tension softening | Simple compression yield surface & the coulomb line | Associated: over predicts inelastic volume strain | Orientation storage of individual cracks, then “plastic “strains of cracks are calculated | Cracks can close completely when stress across them becomes compressive. Not designed for cyclic loading |
MFC [51] | Continuum, smeared cracking. It can be rotating or fixed with more than three cracks and up to a maximum of six cracks per integration point | MCC curves and a selection of tension stiffening or softening curves | Reduces the shear modulus of the concrete by K until the failure limit is reached | Governed by plastic dilatancy, a function of the first strain invariant and K | Makes use of K. Stores the orientation of individual cracks; then, stresses are evaluated in the direction of the respective cracks | The crack reclosing option can be defined |
CDP [52] | Continuum plasticity-based. Fracture energy cracking criterion can be initiated for tensile failure in unreinforced/under-reinforced concrete. | Damaged-elasticity, strain hardening and tension stiffening or softening | Drucker–Prager criteria | Non-associated. Hyperbolic flow potential: fairly accurate | No direct detection. Softening begins beyond tensile failure stress | Compressive stiffness is recoverable upon cracks closure as the loads transition from tensile to compressive. Designed for cyclic loading |
Inner (Layer Volume: 25%,50%,75%) | ||||
---|---|---|---|---|
Outer (layer volume: 25%,50%,75%) | Control (C) | MC-2 | GFC-1 | |
Control | C | Case 1: C_MC-2 | Case 2: C_GFC-1 | |
MC-2 | Case 4: MC-2_C | MC-2 | Case 3: MC-2_GFC-1 | |
GFC-1 | Case 5: GFC-1_C | Case 6: GFC-1_MC-2 | GFC-1 |
Inner (Layer Volume: 33.333% Each) | ||||
---|---|---|---|---|
Outer and mid (layer volume: 33.333% each) | Control (C) | MC-2 | GFC-1 | |
Control_MC-2 | Class 1–Case 1: C_MC-2_C | Class 1–Case 2: MC-2_C_MC-2 | Class 3–Case 3,4: C_MC-2_GFC-1 MC-2_C_GFC-1 | |
Control_GFC-1 | Class 1–Case 5: C_GFC-1_C | Class 4–Case 6,7: C-GFC-1_MC-2 GFC-1_C_MC-2 | Class 2–Case 8: GFC-1_C_GFC-1 | |
MC-2_GFC-1 | Class 5–Case 9,10: MC-2_GFC-1_C GFC-1_MC-2_C | Class 2–Case 11: MC-2_GFC-1_MC-2 | Class 2–Case 12: GFC-1_MC-2_GFC-1 |
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Liu, H.; Egbe, K.-J.I.; Wang, H.; Matin Nazar, A.; Jiao, P.; Zhu, R. A Numerical Study on 3D Printed Cementitious Composites Mixes Subjected to Axial Compression. Materials 2021, 14, 6882. https://doi.org/10.3390/ma14226882
Liu H, Egbe K-JI, Wang H, Matin Nazar A, Jiao P, Zhu R. A Numerical Study on 3D Printed Cementitious Composites Mixes Subjected to Axial Compression. Materials. 2021; 14(22):6882. https://doi.org/10.3390/ma14226882
Chicago/Turabian StyleLiu, Hanqiu, King-James Idala Egbe, Haipeng Wang, Ali Matin Nazar, Pengcheng Jiao, and Ronghua Zhu. 2021. "A Numerical Study on 3D Printed Cementitious Composites Mixes Subjected to Axial Compression" Materials 14, no. 22: 6882. https://doi.org/10.3390/ma14226882
APA StyleLiu, H., Egbe, K. -J. I., Wang, H., Matin Nazar, A., Jiao, P., & Zhu, R. (2021). A Numerical Study on 3D Printed Cementitious Composites Mixes Subjected to Axial Compression. Materials, 14(22), 6882. https://doi.org/10.3390/ma14226882