Compressive failure due to kink band formation in the presence of transverse loading, and accounting for mesoscale and microscale misalignment

2021 ◽  
Vol 265 ◽  
pp. 113760
Author(s):  
Paul Davidson ◽  
Anthony M. Waas
2019 ◽  
Vol 89 (18) ◽  
pp. 3825-3838
Author(s):  
Ahmad Abuobaid ◽  
Raja Ganesh ◽  
John W Gillespie

A dynamic loop test method for measuring strain rate-dependent fiber properties was developed. During dynamic loop testing, the fiber ends are accelerated at constant levels of 20.8, 50 and 343 m/s2. The test method is used to study Kevlar® KM2-600, which fails in axial compression due to kink band formation. The compressive failure strain and strain rate at the onset of kink band formation is calculated from the critical loop diameter ( D C), which is monitored throughout the test using a high-speed camera. The results showed that compressive failure strain increases with strain rates from quasi-static to a maximum strain rate of 116 s−1 by a factor of ∼3. Kink angles (φ) and kink band spacing ( D S) were 60 ° ± 2 ° and 16 ± 3 μm, respectively, over the strain rates tested. Rate-dependent mechanisms of compressive failure by kink band formation were discussed.


Author(s):  
Var L. St. Jeor ◽  
C. C. Chau ◽  
Mark Thomsen

A large portion of the interest currently given high performance polymer fibers stems from their potential use in composite construction. Although many of these fibers display good tensile properties, compressive strength is a major concern. There are many studies which have observed the compressive failure morphology of polymeric fibers. These studies usually involve the postmortem observation of samples which have failed, either partly or completely, following compressive strain. Observations have included such events as kink band formation, brittle failure and other modes as well. But to our knowledge these failure modes have not been recorded, in process, using the scanning electron microscope (SEM). In this article we introduce a technique which allows observation of compressive failure within the SEM, or using light microscopy (LM), in process. We also present some results unique to this procedure. This technique allows us to follow this "process" of compressive failure including both it's initiation and the more advanced stages of failure. Since the compressive failure of polymeric fibers is a process rather than an instantaneous event we have been able to record this process of failure, in it's various stages, in relatively high resolution SEM micrographs. Our methodology involves the use of relatively low accelerating voltages to minimize charging artifacts associated with damaged areas of the fiber. This induced damage can disrupt the 3 - 5nm sputter coating used to prevent such artifact resulting in uncoated fiber being exposed to the electron beam. This technique also lends itself readily to video recording. We have observed compressive failure processes for Kevlar 49®, Spectra 1000®, Hercules AS-4® carbon and various experimental fibers such as Polybenzobisoxazole (PBO). Our observations have included such modes of failure as kink band formation, delamination, buckling and brittle failure. It is noted that some of these processes occur simultaneously in any given fiber, and with the exception of brittle failure, these processes can be recorded at every stage of development visible to the SEM.


Author(s):  
S. T. Pinho ◽  
R. Gutkin ◽  
S. Pimenta ◽  
N. V. De Carvalho ◽  
P. Robinson

Modelling the longitudinal compressive failure of carbon-fibre-reinforced composites has been attempted for decades. Despite many developments, no single model has surfaced to provide simultaneously a definitive explanation for the micromechanics of failure as well as validated predictions for a generic stress state. This paper explores the reasons for this, by presenting experimental data (including scanning electron microscopic observations of loaded kink bands during propagation, and brittle shear fracture at 45 ° to the fibres) and reviewing previously proposed micromechanical analytical and numerical models. The paper focuses mainly on virgin unidirectional (UD) composites, but studies for woven and recycled composites are also presented, highlighting similarities and differences between these cases. It is found that, while kink-band formation (also referred to in the literature as microbuckling) is predominant in UD composites under longitudinal compression, another failure mode related to the failure of the fibres can be observed experimentally. It is also shown that the micromechanics of the failure process observed in UD composites is similar to that in other fibre architectures, hence encouraging the adaptation and application of models developed for the former to the latter.


2018 ◽  
Vol 149 ◽  
pp. 66-73 ◽  
Author(s):  
Vedad Tojaga ◽  
Simon P.H. Skovsgaard ◽  
Henrik Myhre Jensen

1999 ◽  
Author(s):  
Kenji Oguni ◽  
G. Ravichandran

Abstract Results from an experimental investigation on the mechanical behavior of a unidirectional reinforced polymer composite with 50% volume fraction E-glass/vinylester under uniaxial and proportional multiaxial compression are presented. Specimens are loaded in the fiber direction using a servo-hydraulic material testing system for low strain rates and a Kolsky (split Hopkinson) pressure bar for high strain rates, up to 3000 s−1. The results indicate that the compressive strength of the composite increases with increasing levels of confinement and increasing strain rates. Post-test optical and scanning electron microscopy is used to identify the failure modes. The failure mode that is observed in unconfined specimen is axial splitting followed by fiber kink band formation. At high levels of confinement, the failure mode transitions from axial splitting to kink band formation and fiber failure. Also, a new energy based analytic model for studying axial splitting phenomenon in unidirectional fiber-reinforced composites is presented.


2019 ◽  
Vol 809 ◽  
pp. 23-28
Author(s):  
Florian Herrla ◽  
Helmut Rapp

The fatigue behaviour of [0°/±45°] triaxial braided composites is investigated. Tension-tension and compression-compression loading is chosen to study main damage mechanisms and their effect on the stiffness degradation. In both cyclic loading cases a high stiffness degradation can be observed shortly after the start of cyclic loading. Inter-fibre fractures in the braid yarns with subsequent delaminations are responsible for this behaviour during tension-tension loading. Compression-compression loading leads to kink band formation in the axial yarns favoured by yarn undulations. In consequence of the observed material degradation, S-N curves based on a defined level of stiffness degradation are proposed for fatigue dimensioning instead of load cycles to fracture.


2015 ◽  
Vol 21 (S3) ◽  
pp. 1157-1158 ◽  
Author(s):  
T. Nizolek ◽  
N.A. Mara ◽  
R.J. McCabe ◽  
J.T. Avallone ◽  
I.J. Beyerlein ◽  
...  

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