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J. Compos. Sci.
Special Issues
Dynamic Behavior and Failure Analysis of Composites
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Dynamic Behavior and Failure Analysis of Composites

A special issue of Journal of Composites Science (ISSN 2504-477X). This special issue belongs to the section "Composites Manufacturing and Processing".

Deadline for manuscript submissions: closed (30 November 2021) | Viewed by 8961

Special Issue Editor

Prof. Serge Abrate

E-Mail Website
Guest Editor
Department of Mechanical Engineering and Energy Processes, Southern Illinois University at Carbondale, Carbondale, IL, USA
Interests: solid mechanics; advanced materials; vibrations; waves

Special Issue Information

Dear Colleagues,

This Special Issue will focus on the dynamic response and failure of multilayer structures.  Studies of the response of laminated composite structures, sandwich structures, laminated glass, and photovoltaic laminates subjected to blasts, impacts, and other types of dynamic loadings are of interest. Stresses determined on the macroscale (laminate level) are used to predict intra-ply damage and debonding between adjacent plies. The properties of a ply (mesoscale) including damage can be determined by an analysis at the micro-scale (diameter of one reinforcing fiber).  Therefore, the analysis of such problems generally requires a multiscale progressive damage analysis.

Contributions dealing with new plates and shell theories, constitutive equations, damage criteria, cohesive zone models, generalized elasticity theories, and numerical models are welcome.

Prof. Serge Abrate
Guest Editor

Manuscript Submission Information

Manuscripts should be submitted online at www.mdpi.com by registering and logging in to this website. Once you are registered, click here to go to the submission form. Manuscripts can be submitted until the deadline. All submissions that pass pre-check are peer-reviewed. Accepted papers will be published continuously in the journal (as soon as accepted) and will be listed together on the special issue website. Research articles, review articles as well as short communications are invited. For planned papers, a title and short abstract (about 100 words) can be sent to the Editorial Office for announcement on this website.

Submitted manuscripts should not have been published previously, nor be under consideration for publication elsewhere (except conference proceedings papers). All manuscripts are thoroughly refereed through a single-blind peer-review process. A guide for authors and other relevant information for submission of manuscripts is available on the Instructions for Authors page. Journal of Composites Science is an international peer-reviewed open access monthly journal published by MDPI.

Please visit the Instructions for Authors page before submitting a manuscript. The Article Processing Charge (APC) for publication in this open access journal is 1800 CHF (Swiss Francs). Submitted papers should be well formatted and use good English. Authors may use MDPI's English editing service prior to publication or during author revisions.

Keywords

  • Composites
  • Sandwich
  • Dynamics
  • Impact
  • Blast
  • Beams
  • Plates
  • Shells
  • Damage
  • Contact

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Published Papers (3 papers)

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Research

11 pages, 4009 KiB  
Article
Evaluating Impact Damage of Flat Composite Plate for Surrogate Bird-Strike Testing of Aeroengine Fan Blade
by Youchao Sun, Yuemei Zhang, Yadong Zhou, Haitao Zhang, Haijun Zeng and Kun Yang
J. Compos. Sci. 2021, 5(7), 171; https://doi.org/10.3390/jcs5070171 - 30 Jun 2021
Cited by 11 | Viewed by 3153
Abstract
Bird-strike failure of fan blades is one of the basic challenges for the safety of aircraft engines. Simplified flat blade-like plates are always used for damage mechanism study of composite laminates. One undesirable issue is the failure at the root of clamped flat [...] Read more.
Bird-strike failure of fan blades is one of the basic challenges for the safety of aircraft engines. Simplified flat blade-like plates are always used for damage mechanism study of composite laminates. One undesirable issue is the failure at the root of clamped flat plates under high-velocity impact. For this purpose, two different strategies were exploited to obtain desirable impact damage distributions, namely the impact location and the boundary condition. Numerical models of the simplified flat blade-like plate and the bird projectile were constructed by using finite element method (FEM) and smoothed particle hydrodynamics (SPH) approaches. The impact damage distributions were comparatively investigated in detail. The numerical results show that changing the boundary condition is the most effective way to obtain preferable impact damages for further failure analysis of real fan blades. Present results will be useful to the future surrogate experimental design of simplified bird-strike testing. Full article
(This article belongs to the Special Issue Dynamic Behavior and Failure Analysis of Composites)
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17 pages, 5761 KiB  
Article
Effect of Defects Part II: Multiscale Effect of Microvoids, Orientation of Rivet Holes on the Damage Propagation, and Ultimate Failure Strength of Composites
by Vahid Tavaf, Mohammadsadegh Saadatzi and Sourav Banerjee
J. Compos. Sci. 2021, 5(4), 112; https://doi.org/10.3390/jcs5040112 - 17 Apr 2021
Cited by 5 | Viewed by 2425
Abstract
Material properties at the vicinity of the cut-outs in composites are not entirely defect-free. The nteraction of multiple cutouts like rivet holes, the repercussion of their configuration on crack propagation, and ultimate strength were predicted using Peridynamic method and the results are reported [...] Read more.
Material properties at the vicinity of the cut-outs in composites are not entirely defect-free. The nteraction of multiple cutouts like rivet holes, the repercussion of their configuration on crack propagation, and ultimate strength were predicted using Peridynamic method and the results are reported in this article. The effect of microscale defects at the vicinity of the cutouts on macroscale damage propagation were shown to have quantifiable manifestation. This study focused on two to four holes in unidirectional composite plates with 0°, 45°, and 90° fiber directions, while the vicinity of a hole was considered degraded. Numerical results were validated using quantitative ultrasonic image correlation (QUIC) and the tensile test. Both the experimental and numerical results confirmed that the strength of the horizontal configuration is higher than the vertical in the plates with two holes. Furthermore, the square configuration was found to be stronger than the diamond configuration with four holes. When the effect of microscale defects was considered, the prediction of ultimate strength was better compared to the experimental results. The predictive model could be reliably used for progressive damage analysis. Full article
(This article belongs to the Special Issue Dynamic Behavior and Failure Analysis of Composites)
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24 pages, 11996 KiB  
Article
Effect of Structural Parameters on the Deformational Behaviors of Multiply 3D Layer-by-Layer Angle-Interlock Para-Aramid Fabric for Fiber-Reinforcement Composite
by Mulat Alubel Abtew, Francois Boussu, Pascal Bruniaux, Carmen Loghin and Irina Cristian
J. Compos. Sci. 2020, 4(4), 145; https://doi.org/10.3390/jcs4040145 - 24 Sep 2020
Cited by 4 | Viewed by 2816
Abstract
Materials used in the technical application including composite reinforcements and ballistic fabrics should show not only good mechanical performance but also better deformational behaviors. Meanwhile, three dimensional (3D) warp interlock fabrics have been widely employed in such applications to substitute the two dimensional [...] Read more.
Materials used in the technical application including composite reinforcements and ballistic fabrics should show not only good mechanical performance but also better deformational behaviors. Meanwhile, three dimensional (3D) warp interlock fabrics have been widely employed in such applications to substitute the two dimensional (2D) fabrics because of their enhanced through-the-thickness performance and excellent formability. The deformational behaviors of such 3D warp interlock fabrics have been also influenced by various internal and external parameters. To understand and fill this gap, the current paper investigates the effects of the warp yarn interchange ratios inside the fabric structure on the formability behaviors of dry 3D warp interlock p-aramid fabrics. Four 3D warp interlock architecture types made with different binding and stuffer warp yarn interchange ratios were designed and manufactured. An adapted hydraulic-driven stamping bench along with hemispherical punch was utilized for better forming behavior analysis such as in-plane shear angle and its recovery, material drawing-in and its recovery, deformational depth recovery, and required stamping forces. Based on the investigation of various formability behaviors, the formability of (3D) warp interlock fabrics were greatly influenced by the binding and stuffer warp yarns interchange ratio inside the 3D warp interlock structure. For example, preform 3D-8W-0S exhibited a maximum deformational height recovery percentage of 5.1%, whereas 3D-4W-8S recorded only 0.72%. Preform 3D-8W-4S and 3D-8W-8S revealed 1.45% and 4.35% recovery percentages toward the deformational height at maximum position. Besides, sample 3D-4S-8W revealed the maximum drawing-in recovery percentage of 43.13% and 46.98% in the machine and cross direction, respectively, around the preform peripheral edges. On the contrary, samples with higher binding warp yarns as 3D-8W-0S show the maximum drawing-in recovery percentages values of 31.21% and 34.99% in the machine and cross directions respectively. Full article
(This article belongs to the Special Issue Dynamic Behavior and Failure Analysis of Composites)
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