1. Experimental And Numerical Assessment Of The Improvement Of The Load-Carrying Capacities Of Butterfly-Shaped Coupling Components In Composite Structures
- Author
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Muzaffer Topcu and Guerkan Altan
- Subjects
Materials science ,Composite number ,Experimental studies ,Life span ,Geometry ,Modified model ,Span (engineering) ,Joint failure ,Structure (composition) ,Coupling geometry ,Load carrying capacities ,New results ,Coupling component ,Coupling ,Numerical and experimental study ,Specimen width ,business.industry ,Mechanical Engineering ,Numerical analysis ,Water jet ,Numerical assessment ,Structural engineering ,Concrete beams and girders ,Load carrying ,Failure load ,Butterfly joint ,Machine components ,Numerical studies ,Mechanics of Materials ,Water jets ,Butterfly ,business - Abstract
This study was designed to analyze the load-carrying capacities of composite structures connected face-to-face by a butterfly coupling component experimentally and numerically without adhesive. The results of the experimental studies were supported with numerical analysis. In addition, the butterfly coupling component was developed geometrically with a view to the results of the numerical and experimental studies. The change in the load-carrying capacity of the improved butterfly coupling components was analyzed numerically and experimentally to obtain new results. Half-specimens and butterfly-shaped lock components were cut with a water jet machine. Experiments and analyses were conducted to analyze the effects of coupling geometry parameters, such as the ratio of the butterfly end width to the specimen width (w/b), the ratio of the butterfly middle width to the butterfly end width (x/w), and the ratio of the butterfly half height to the specimen width (y/b). It was intended to determine the damage in the butterfly before any damage to the composite structure and to increase the service-life span of the composite structure with the repair of the butterfly lock. As a result of this study, it was determined that the geometrical fixed ratios (w/b) and (x/w) were 0.4 and 0.2 at 0.4 of (y/b) according to the experimental and numerical studies with basic and modified models. © 2010 The Korean Society of Mechanical Engineers and Springer-Verlag Berlin Heidelberg.
- Published
- 2010