Flexural Behaviour of Multi-directional Glass/Carbon Hybrid Laminates

1989 ◽  
pp. 795-807 ◽  
Author(s):  
G. Kretsis ◽  
F. L. Matthews ◽  
G. A. O. Davies ◽  
J. Morton
Keyword(s):  
Flexural Behaviour ◽  
Glass Carbon ◽  
Hybrid Laminates

Experimental Investigation on Static Mechanical Properties of Glass/Carbon Hybrid Woven Fabric Composite Laminates

2014 ◽  
Vol 903 ◽  
pp. 96-101 ◽  
Author(s):  
R. Murugan ◽  
R. Ramesh ◽  
K. Padmanabhan ◽  
R. Jeyaraam ◽  
S. Krishna
Keyword(s):  
Mechanical Properties ◽  
Composite Laminates ◽  
Weight Ratio ◽  
Woven Fabric ◽  
Specific Strength ◽  
Nominal Size ◽  
Glass Carbon ◽  
Hybrid Laminates ◽  
Static Mechanical ◽  
Aircraft Application

Woven fabric reinforced polymeric composites are increasingly used in automotive and aircraft application in place of conventional metals due to their high specific strength. However in actual practice while using glass fabric layers, the large nominal size of the component was required and which facilitates increased total weight of the component. In the present investigation, glass laminate is modified and strengthened by interplying high modulus carbon fiber plies for attaining good strength to weight ratio. All laminates were fabricated using hand layup method. Mechanical properties such as tensile, flexural and impact strengths of dedicated and hybrid laminates were evaluated and reported.

Tailor Made Hybrid Laminates Based on UD-Tapes - A Way to Efficient Thermoplastic Components

2019 ◽  
Vol 809 ◽  
pp. 41-46
Author(s):  
Franz Habla ◽  
M. Kropka ◽  
M. Muehlbacher ◽  
T. Neumeyer ◽  
Volker Altstädt
Keyword(s):  
Carbon Fiber ◽  
Flexural Strength ◽  
Hybrid Material ◽  
Flexural Modulus ◽  
Constant Thickness ◽  
Flexural Properties ◽  
Glass Carbon ◽  
Hybrid Laminates

In this study, the quality of pre-consolidation of a PA6 based glass/carbon hybrid and a glass mono-material UD-tape laminate has been analyzed and the influence of the pre-consolidation step on flexural properties of end-consolidated laminates was determined. For this reason, three different pre-consolidation qualities were mechanically and optically analyzed. The investigations show that the quality of pre-consolidation is not critical for mono-material lay-ups considered in this work. However, the pre-consolidation step has a significant effect on the flexural properties of the hybrid-material laminate presented in this work. The flexural modulus is increased by more than 25 % and the flexural strength up to 9 % due to better welding of the distinct layers. Additionally, the influence of carbon fiber share on the flexural modulus of the UD hybrid-material was examined. It could be recognized that the flexural modulus can be increased up to 171 % by the exchange of glass with carbon fiber layers with a sandwich stacking compared to glass mono-material with constant thickness.

Effect of Accelerated Ageing on Hardness and Flexural Behaviour of Woven fabric Glass/ Carbon Hybrid Epoxy Composites

2017 ◽  
Vol 4 (10) ◽  
pp. 10751-10756
Author(s):  
S. Sunil Kumar ◽  
Neelakantha V. Londe ◽  
A.S. Saviraj ◽  
Vikranth Kannanth
Keyword(s):  
Woven Fabric ◽  
Epoxy Composites ◽  
Accelerated Ageing ◽  
Flexural Behaviour ◽  
Glass Carbon

scholarly journals Wrinkle measurement in glass-carbon hybrid laminates comparing ultrasonic techniques: A case study

2018 ◽  
Vol 114 ◽  
pp. 225-240 ◽  
Author(s):  
Beatriz Larrañaga-Valsero ◽  
Robert A. Smith ◽  
Rostand B. Tayong ◽  
Antonio Fernández-López ◽  
Alfredo Güemes
Keyword(s):  
Glass Carbon ◽  
Hybrid Laminates ◽  
Ultrasonic Techniques

scholarly journals Flexural Behaviour of CFRP/MG Hybrid Laminates with Different Layers Thickness

2017 ◽  
Vol 26 (5) ◽  
pp. 096369351702600 ◽  
Author(s):  
Xuan Wu ◽  
Yingcai Pan ◽  
Guoqing Wu ◽  
Zheng Huang ◽  
Rui Tian ◽  
...  
Keyword(s):  
Layer Thickness ◽  
Volume Fraction ◽  
Flexural Modulus ◽  
Test Method ◽  
Flexural Behaviour ◽  
Compression Region ◽  
Carbon Fibre Reinforced Polymer ◽  
Metal Volume ◽  
Hybrid Laminates ◽  
Fibre Reinforced Polymer

Three different types of fibre metal laminates (FMLs) with varying layers thickness, consisting of carbon fibre reinforced polymer (CFRP) prepregs and magnesium alloy sheets, were prepared by a hot-press process. The flexural behaviour of the FMLs were investigated using a three point flexural test method, to investigate the effect of layer thickness on flexural behaviour of FMLs while maintaining a constant metal volume fraction and constant overall thickness in the design process. The results show that the flexural modulus of the FMLs decreases in an almost linear manner with the decrease of layer thicknesses, yet no clear differences were observed in the flexural strength. Decreasing the layer thickness causes the transition of failure zone from compression region to tension region, which results in the appearance of two similar peak stresses.

Experimental investigation of notch effect and ply number on mechanical behavior of interply hybrid laminates (glass/carbon/epoxy)

2018 ◽  
Vol 145 ◽  
pp. 189-196 ◽  
Author(s):  
Leila Belgacem ◽  
Djamel Ouinas ◽  
Jaime Aurelio Viña Olay ◽  
Antonio Argüelles Amado
Keyword(s):  
Experimental Investigation ◽  
Mechanical Behavior ◽  
Notch Effect ◽  
Glass Carbon ◽  
Hybrid Laminates

scholarly journals Experimental impact study on unidirectional glass-carbon hybrid composite laminates

2016 ◽  
Vol 23 (6) ◽  
pp. 721-728
Author(s):  
A. Arockia Julias ◽  
Vela Murali
Keyword(s):  
Carbon Fiber ◽  
Hybrid Composite ◽  
Composite Laminates ◽  
Unidirectional Glass ◽  
Unidirectional Hybrid ◽  
Glass Carbon ◽  
Time Histories ◽  
Hybrid Laminates ◽  
Unidirectional Hybrid Composite ◽  
The Impact

AbstractIn this experimental study, the impact response of unidirectional hybrid composite laminate was investigated. Hybrid laminates with different stacking sequences were fabricated, using unidirectional glass and carbon fiber as reinforcement and epoxy resin as matrix. ASTM standard D5628 was followed to conduct the experiment using the instrumented drop weight impact test apparatus. All the square specimens were tested at an impact velocity of 3.43 m/s and the time histories of force and energy absorbed were recorded. The impacted specimens and their X-ray images were visually inspected to understand the failure pattern. The experimental results showed that the addition of carbon fiber increases the impact strength by absorbing more force and energy. Furthermore, the laminate can be stiffened with the carbon fiber layers by interfacing glass fiber layers on either side.

scholarly journals Experimental on Flexural Strength of Glass/Kevlar and Glass/Carbon Hybrid Composite Laminates

2019 ◽  
Vol 8 (12S) ◽  
pp. 45-48
Keyword(s):  
Flexural Strength ◽  
Hybrid Composite ◽  
Composite Laminates ◽  
Experimental Results ◽  
Bending Test ◽  
Three Point Bending ◽  
Stacking Order ◽  
Glass Carbon ◽  
Hybrid Laminates

our present study deals with the investigation of flexural strength of Glass/Kevlar epoxy and glass/carbon epoxy hybrid laminates. Laminates of different stacking order were prepared and three point bending test were conducted on the hybrid laminates. From the experimental results, the flexural strength of different hybrid laminates was evaluated and comparisons were made.

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