Experimental and simulation studies on flexural strength of laminated glass using ring-on-ring and three-point bending test

Author(s):  
Ajitanshu Vedrtnam ◽  
SJ Pawar

Flexural strength of laminated glass is noteworthy in architectural, glazing, automotive safety, photo-voltaic, and decorative applications. The flexural strength of laminated glass samples having polyvinyl butyral/ethyl vinyl acetate interlayer of different critical thickness (0.38/0.76/1.52 mm) was determined by ring-on-ring test following the ASTM C1499-15 and also by three-point bending test (for an interlayer of 0.38 mm thickness) following the ASTM D790-03. The effect of inter-layer type and inter-layer thickness on flexural strength is evidently reported from this brief study. The significance F-statics value during regression analysis shows the strong association of flexural strength with inter-layer types and inter-layer thickness, and P-value shows that the error in the analysis is within considerable limits. It is also concluded that the laminated glass samples with polyvinyl butyral interlayer have comparatively lower load capacity than laminated glass samples with ethyl vinyl acetate interlayer for same interlayer and glass thickness. The inter-layer thickness has more prominent role in the determination of load capacity in case of ethyl vinyl acetate laminated glass samples. There is an increment in average load capacity with an increment in critical inter-layer thickness in laminated glass. A finite element analysis is also carried out for simulating the experimentation and obtaining the variation of displacements in the laminated glass samples at their load capacity. The output of the finite element analysis fairly describes the fracture pattern (based on deformation and stress) of the laminated glass samples. The conclusions may be utilized for the selection of suitable laminated glass and predicting failure of laminated glass while used in various structural, automotive and other applications.

Materials ◽  
2019 ◽  
Vol 12 (14) ◽  
pp. 2241 ◽  
Author(s):  
Tomáš Hána ◽  
Tomáš Janda ◽  
Jaroslav Schmidt ◽  
Alena Zemanová ◽  
Michal Šejnoha ◽  
...  

An accurate material representation of polymeric interlayers in laminated glass panes has proved fundamental for a reliable prediction of their response in both static and dynamic loading regimes. This issue is addressed in the present contribution by examining the time–temperature sensitivity of the shear stiffness of two widely used interlayers made of polyvinyl butyral (TROSIFOL BG R20) and ethylene-vinyl acetate (EVALAM 80-120). To that end, an experimental program has been executed to compare the applicability of two experimental techniques, (i) dynamic torsional tests and (ii) dynamic single-lap shear tests, in providing data needed in a subsequent calibration of a suitable material model. Herein, attention is limited to the identification of material parameters of the generalized Maxwell chain model through the combination of linear regression and the Nelder–Mead method. The choice of the viscoelastic material model has also been supported experimentally. The resulting model parameters confirmed a strong material variability of both interlayers with temperature and time. While higher initial shear stiffness was observed for the polyvinyl butyral interlayer in general, the ethylene-vinyl acetate interlayer exhibited a less pronounced decay of stiffness over time and a stiffer response in long-term loading.


Author(s):  
M.R. Ashok ◽  
M. Manojkumar ◽  
P.V. Inbanaathan ◽  
R. Shanmuga Prakash

This paper details the fabrication and flexural testing of sandwich structure with Aluminium honeycomb core with Aluminium face skins. The material for the face skin is aluminium 1100 and for the core is Aluminium AA8011. The cell size obtained by fabrication is 7mm. The specimen is prepared and tested as per the ASTM standard C393/C393M-11 on a three-point bending test to obtain the ultimate core shear strength and the face skin strength. Finite element analysis is also carried out to validate the experimental test.


2007 ◽  
Vol 14 (04) ◽  
pp. 817-820
Author(s):  
MIN HUANG ◽  
KE-ZHI LI ◽  
HE-JUN LI ◽  
QIAN-GANG FU ◽  
GUO-DONG SUN

SiC coating for carbon/carbon composites was prepared by pack cementation method. The effects of coating process on the microstructure and the mechanical properties of C / C composites were analyzed by SEM and three-point bending test, respectively. As the infiltrated Si improved the interfaces bonding during the coating process, the flexural strength and flexural modulus of SiC -coated carbon/carbon composites were both increased by about 10% than the naked C / C composites. In addition, the mechanism of the change of failure mode of SiC coated C / C composites and naked C / C composites was addressed.


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