| contributor author | Yu Bai | |
| contributor author | Xiao Yang | |
| date accessioned | 2017-05-08T21:36:35Z | |
| date available | 2017-05-08T21:36:35Z | |
| date copyright | February 2013 | |
| date issued | 2013 | |
| identifier other | %28asce%29cc%2E1943-5614%2E0000307.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/57440 | |
| description abstract | A space truss is formed of interconnected structural components that transfer loads axially. Pultruded glass-fiber reinforced polymer (GFRP) composites exhibit their best material strength in the axial (pultrusion) direction, and their inherent lack of material stiffness can be compensated by the structural stiffness achieved by space configuration. A novel connector made of pultruded GFRP profiles is proposed in this paper to join diagonal and chord members and to form all-composite free-form space trusses. The proposed truss unit was assembled and tested statically, and the load-displacement responses were recorded. The final collapse of the structural unit evidenced a pull-out shear failure mode in the bolt connections, and the ultimate load can therefore be well predicted by this mechanism. A detailed finite element (FE) analysis considering the interaction between the bolts and FRP profiles was conducted for the structural unit to investigate the effects of pretension force of bolted connections and the stress concentration at the joint region. A simplified FE approach was used to demonstrate one- and two-dimensional space trusses with satisfactory structural stiffnesses. | |
| publisher | American Society of Civil Engineers | |
| title | Novel Joint for Assembly of All-Composite Space Truss Structures: Conceptual Design and Preliminary Study | |
| type | Journal Paper | |
| journal volume | 17 | |
| journal issue | 1 | |
| journal title | Journal of Composites for Construction | |
| identifier doi | 10.1061/(ASCE)CC.1943-5614.0000304 | |
| tree | Journal of Composites for Construction:;2013:;Volume ( 017 ):;issue: 001 | |
| contenttype | Fulltext | |