Author Contributions
Conceptualization, F.T., W.Z. and B.M.; Methodology, F.T., W.Z. and B.M.; Software, F.T., W.Z. and B.M.; Validation, F.T., W.Z. and B.M.; Formal analysis, F.T., W.Z. and B.M.; Investigation, F.T., W.Z. and B.M.; Resources, F.T. and K.S.; Data curation, W.Z., B.M. and K.S.; Writing—original draft, F.T, W.Z. and B.M.; Writing—review & editing, F.T. and K.S.; Supervision, K.S.; Project administration, K.S. All authors have read and agreed to the published version of the manuscript.
Figure 1.
Isometric of a bamboo culm (left) and isometric of timber beam (right) showing a similar composition in the direction of the fibers/grain, though with different cross-sections.
Figure 1.
Isometric of a bamboo culm (left) and isometric of timber beam (right) showing a similar composition in the direction of the fibers/grain, though with different cross-sections.
Figure 2.
Bamboo connection by the mortise and tenon joint (a,c) and bundling with bolted connections (b).
Figure 2.
Bamboo connection by the mortise and tenon joint (a,c) and bundling with bolted connections (b).
Figure 3.
Annotated high-level study of structural actions in design.
Figure 3.
Annotated high-level study of structural actions in design.
Figure 4.
Annotated high-level study of structural actions in design.
Figure 4.
Annotated high-level study of structural actions in design.
Figure 5.
Annotated high-level study of structural actions in design.
Figure 5.
Annotated high-level study of structural actions in design.
Figure 7.
Elevation and plan view of Design Iteration One.
Figure 7.
Elevation and plan view of Design Iteration One.
Figure 8.
Visualization of Design Iteration Three (c) in comparison to previous iterations (a,b).
Figure 8.
Visualization of Design Iteration Three (c) in comparison to previous iterations (a,b).
Figure 10.
Axonometric model of Iteration One (a) with exploded view of structure (b).
Figure 10.
Axonometric model of Iteration One (a) with exploded view of structure (b).
Figure 11.
Plan (a) and elevation (b) view of Iteration Two.
Figure 11.
Plan (a) and elevation (b) view of Iteration Two.
Figure 12.
Axonometric model of Iteration Two.
Figure 12.
Axonometric model of Iteration Two.
Figure 13.
Plan (a) and elevation (b) view of Iteration Two.
Figure 13.
Plan (a) and elevation (b) view of Iteration Two.
Figure 14.
Axonometric model of Iteration Three.
Figure 14.
Axonometric model of Iteration Three.
Figure 15.
Plan (a) and elevation (b) view of Iteration Three.
Figure 15.
Plan (a) and elevation (b) view of Iteration Three.
Figure 16.
Massing model (a), divided surfaces (b), and structural model (c) of Case Study One.
Figure 16.
Massing model (a), divided surfaces (b), and structural model (c) of Case Study One.
Figure 17.
Massing model (a) and divided surfaces (b) of Case Study Two.
Figure 17.
Massing model (a) and divided surfaces (b) of Case Study Two.
Figure 18.
Strand7 analysis of Case Study One—Iteration One showing the deformed shape of the combined structural system (a). An isolated analysis was conducted for the structural beams (b) and plywood cladding system (c).
Figure 18.
Strand7 analysis of Case Study One—Iteration One showing the deformed shape of the combined structural system (a). An isolated analysis was conducted for the structural beams (b) and plywood cladding system (c).
Figure 19.
Strand7 analysis of Case Study One—Iteration One showing the maximum fiber stresses of bamboo beams of the combined structural system showing the deformed shape (a) and fiber stresses by cross-sectional area (b).
Figure 19.
Strand7 analysis of Case Study One—Iteration One showing the maximum fiber stresses of bamboo beams of the combined structural system showing the deformed shape (a) and fiber stresses by cross-sectional area (b).
Figure 20.
Strand7 analysis of Case Study One—Iteration Two showing the deformed shape of the combined structural system (a). An isolated analysis was conducted for the structural beams (b) and plywood cladding system (c).
Figure 20.
Strand7 analysis of Case Study One—Iteration Two showing the deformed shape of the combined structural system (a). An isolated analysis was conducted for the structural beams (b) and plywood cladding system (c).
Figure 21.
Strand7 analysis of Case Study One—Iteration Two showing the maximum fiber stresses of bamboo beams of the combined structural system showing the deformed shape (a) and fiber stresses by cross-sectional area (b).
Figure 21.
Strand7 analysis of Case Study One—Iteration Two showing the maximum fiber stresses of bamboo beams of the combined structural system showing the deformed shape (a) and fiber stresses by cross-sectional area (b).
Figure 22.
Strand7 analysis of Case Study One—Iteration Three showing the deformed shape of the combined structural system (a). An isolated analysis was conducted for the structural beams (b) and plywood cladding system (c).
Figure 22.
Strand7 analysis of Case Study One—Iteration Three showing the deformed shape of the combined structural system (a). An isolated analysis was conducted for the structural beams (b) and plywood cladding system (c).
Figure 23.
Strand7 analysis of Case Study One—Iteration Three showing the maximum fiber stresses of bamboo beams of the combined structural system showing the deformed shape (a) and fiber stresses by cross-sectional area (b).
Figure 23.
Strand7 analysis of Case Study One—Iteration Three showing the maximum fiber stresses of bamboo beams of the combined structural system showing the deformed shape (a) and fiber stresses by cross-sectional area (b).
Figure 24.
Additional Strand7 Analysis of deflection of bamboo beams system showing the deformed shape (a) compared to the combined cladding and beams structural system (b).
Figure 24.
Additional Strand7 Analysis of deflection of bamboo beams system showing the deformed shape (a) compared to the combined cladding and beams structural system (b).
Figure 25.
Strand7 analysis of Case Study Two—Iteration One showing the most critical deformed shape of the combined structural system, under load case G + 0.7Q + W.
Figure 25.
Strand7 analysis of Case Study Two—Iteration One showing the most critical deformed shape of the combined structural system, under load case G + 0.7Q + W.
Figure 26.
Strand7 analysis of Case Study Two—Iteration One showing the maximum fiber stresses of bamboo beams of the combined structural system showing the deformed shape under wind load (a) and fiber stresses by cross-sectional area (b).
Figure 26.
Strand7 analysis of Case Study Two—Iteration One showing the maximum fiber stresses of bamboo beams of the combined structural system showing the deformed shape under wind load (a) and fiber stresses by cross-sectional area (b).
Figure 27.
Strand7 analysis of Case Study Two—Iteration Two showing the most critical deformed shape of the combined structural system, under load case 1.2G + 1.5Q.
Figure 27.
Strand7 analysis of Case Study Two—Iteration Two showing the most critical deformed shape of the combined structural system, under load case 1.2G + 1.5Q.
Figure 28.
Strand7 analysis of Case Study Two—Iteration Two showing the maximum fiber stresses of bamboo beams of the combined structural system showing the deformed shape under wind load (a) and fiber stresses by cross-sectional area (b).
Figure 28.
Strand7 analysis of Case Study Two—Iteration Two showing the maximum fiber stresses of bamboo beams of the combined structural system showing the deformed shape under wind load (a) and fiber stresses by cross-sectional area (b).
Figure 29.
Strand7 analysis of Case Study Two—Iteration Three showing the most critical deformed shape of the combined structural system, under load case 1.2G + W + Q.
Figure 29.
Strand7 analysis of Case Study Two—Iteration Three showing the most critical deformed shape of the combined structural system, under load case 1.2G + W + Q.
Figure 30.
Strand7 analysis of Case Study Two—Iteration Three showing the maximum fiber stresses of bamboo beams of the combined structural system showing the deformed shape under wind load (a) and fiber stresses by cross-sectional area (b).
Figure 30.
Strand7 analysis of Case Study Two—Iteration Three showing the maximum fiber stresses of bamboo beams of the combined structural system showing the deformed shape under wind load (a) and fiber stresses by cross-sectional area (b).
Figure 31.
Comparison of deflections (along the z-direction) between each design.
Figure 31.
Comparison of deflections (along the z-direction) between each design.
Figure 32.
Comparison of fiber stresses (along the y-direction) of each design.
Figure 32.
Comparison of fiber stresses (along the y-direction) of each design.
Figure 33.
Comparison of deflections (along the z-direction) between each design.
Figure 33.
Comparison of deflections (along the z-direction) between each design.
Figure 34.
Comparison of axial stresses (along the z-direction) between each design.
Figure 34.
Comparison of axial stresses (along the z-direction) between each design.
Figure 35.
Comparison of fiber stresses (along the y-direction) between each design.
Figure 35.
Comparison of fiber stresses (along the y-direction) between each design.
Table 1.
Comparison of raw bamboo and bamboo scrimber properties.
Table 1.
Comparison of raw bamboo and bamboo scrimber properties.
| Raw Bamboo | Bamboo Scrimber |
---|
Material Properties | Anisotropic and non-homogeneous | Isotropic and homogeneous |
Cost | In-expensive | Larger due to manufacturing |
Curvature | Harder to form curves | Easier to form curves |
Density ρ (kg/m3) | 666 [9] | 1010 |
Compression fc (Mpa) | 53 [9] | 134.9 |
Tension ft (Mpa) | 153 [9] | 296.2 |
Shear τ (Mpa) | 16 [9] | 15 |
Flexural fb (Mpa) | 135 [9] | 119 |
Elastic Young’s Modulus (GPa) | 15 [9] | 22.9 |
Poisson’s Ratio | 0.52 [9] | 0.22 |
Table 2.
Material properties.
Table 2.
Material properties.
Property | Value | Units |
---|
Density (⍴) | 666 [9] | kg/m3 |
Elastic Modulus | 15 [9] | GPa |
Poisson’s Ratio | 0.46 [9] | - |
Diameter (D) | 0.07 [24] | m |
Thickness (t) | 0.012 [26] | m |
Table 3.
Values of gravity and wind loads for FEA Analysis.
Table 3.
Values of gravity and wind loads for FEA Analysis.
Load Types | Value | Units |
---|
Dead Loads (D) [26] | 0.47 | kPa |
Live Loads (Q) | 0.25 | kPa |
Wind Loads (W) | 1.0 | kPa |
Table 4.
Loading Cases to be used for FEA Analysis.
Table 4.
Loading Cases to be used for FEA Analysis.
Criteria | Load Combination |
---|
Serviceability Limit State | G + Q |
G + 0.7Q + W |
Ultimate Limit State | 1.35 G |
1.2G + 1.5Q |
1.2G + W + Q |
Table 5.
Design Criteria for Case One—Buddhist Lotus Shelter.
Table 5.
Design Criteria for Case One—Buddhist Lotus Shelter.
Criteria | Limit | Units |
---|
Deflection Limit | 40 | mm |
Axial (Compressive) Stress Limit | 43.7 | MPa |
Axial (Tensile) Stress Limit | 43.7 | MPa |
Fibre Stress Limit | 26.1 | MPa |
Table 6.
Design Criteria for Case Study Two—Modular Community Pavilion.
Table 6.
Design Criteria for Case Study Two—Modular Community Pavilion.
Criteria | Limit | Units |
---|
Deflection Limit | 26.15 | mm |
Axial (Compressive) Stress Limit | 108 | MPa |
Axial (Tensile) Stress Limit | 115 | MPa |
Fibre Stress Limit | 43.5 | MPa |
Table 7.
Tensile and compressive fiber stresses for Case Study One—Iteration One.
Table 7.
Tensile and compressive fiber stresses for Case Study One—Iteration One.
| Tension Stress | Compression Stress |
---|
Failure Stresses (kPa) | 43,500 | 43,500 |
Design Stresses (kPa) | 1580 | 2073 |
Utilized Ratio | 3.6% | 4.8% |
Table 8.
Tensile and compressive fiber stresses for Case Study One—Iteration Two.
Table 8.
Tensile and compressive fiber stresses for Case Study One—Iteration Two.
| Tension Stress | Compression Stress |
---|
Failure Stresses (kPa) | 43,500 | 43,500 |
Design Stresses (kPa) | 12,030 | 11,810 |
Utilization Ratio | 27.7% | 27.1% |
Table 9.
Tensile and compressive fiber stresses for Case Study One—Iteration Three.
Table 9.
Tensile and compressive fiber stresses for Case Study One—Iteration Three.
| Tension Stress | Compression Stress |
---|
Failure Stresses (kPa) | 43,500 | 43,500 |
Design Stresses (kPa) | 19,006 | 19,600 |
Utilized Ratio | 43.7% | 45.5% |
Table 10.
Tensile and Compressive fiber stresses for Case Study Two—Iteration One.
Table 10.
Tensile and Compressive fiber stresses for Case Study Two—Iteration One.
| Tension Stress | Compression Stress |
---|
Failure Stresses (kPa) | 43,500 | 43,500 |
Design Stresses (kPa) | 42,201 | 65,106 |
Utilization Ratio | 97% | 150% |
Table 11.
Tensile and compressive fiber stresses for Case Study Two—Iteration One.
Table 11.
Tensile and compressive fiber stresses for Case Study Two—Iteration One.
| Tension Stress | Compression Stress |
---|
Failure Stresses (kPa) | 43,500 | 43,500 |
Design Stresses (kPa) | 21,272 | 43,663 |
Utilization Ratio | 49% | 100% |
Table 12.
Tensile and compressive fiber stresses for Case Study Two—Iteration One.
Table 12.
Tensile and compressive fiber stresses for Case Study Two—Iteration One.
| Tension Stress | Compression Stress |
---|
Failure Stresses (kPa) | 43,500 | 43,500 |
Design Stresses (kPa) | 245 | 211 |
Utilization Ratio | 0.56% | 0.49% |