text:
@article{ ISI:000321422200003,
Author = {Brantut, N. and Heap, M. J. and Meredith, P. G. and Baud, P.},
Title = {{Time-dependent cracking and brittle creep in crustal rocks: A review}},
Journal = {{JOURNAL OF STRUCTURAL GEOLOGY}},
Year = {{2013}},
Volume = {{52}},
Pages = {{17-43}},
Month = {{JUL}},
Abstract = {{Rock fracture under upper crustal conditions is driven not only by
   applied stresses, but also by time-dependent, chemically activated
   subcritical cracking processes. These subcritical processes are of great
   importance for the understanding of the mechanical behaviour of rocks
   over geological timescales. A macroscopic manifestation of
   time-dependency in the brittle field is the observation that rocks can
   deform and fail at constant applied stresses, a phenomenon known as
   brittle creep. Here, we review the available experimental evidence for
   brittle creep in crustal rocks, and the various models developed to
   explain the observations. Laboratory experiments have shown that brittle
   creep occurs in all major rock types, and that creep strain rates are
   extremely sensitive to the environmental conditions: differential
   stress, confining pressure, temperature and pore fluid composition. Even
   small changes in any of these parameters produce order of magnitude
   changes in creep strain rates (and times-to-failure). Three main classes
   of brittle creep model have been proposed to explain these observations:
   phenomenological, statistical, and micromechanical. Statistical and
   micromechanical models explain qualitatively how the increasing
   influence of microcrack interactions and/or the increasing accumulated
   damage produces the observed evolution of macroscopic deformation during
   brittle creep. However, no current model can predict quantitatively all
   of the observed features of brittle creep. Experimental data are limited
   by the timescale over which experiments are realistically feasible.
   Clearly, an extension of the range of available laboratory data to lower
   strain rates, and the development of new modelling approaches are needed
   to further improve our current understanding of time-dependent brittle
   deformation in rocks. Crown Copyright (C) 2013 Published by Elsevier
   Ltd. All rights reserved.}},
Publisher = {{PERGAMON-ELSEVIER SCIENCE LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, ENGLAND}},
Type = {{Review}},
Language = {{English}},
Affiliation = {{Brantut, N (Reprint Author), UCL, Dept Earth Sci, RIPL, Gower St, London WC1E 6BT, England.
   Brantut, N.; Meredith, P. G., UCL, Dept Earth Sci, RIPL, London WC1E 6BT, England.
   Heap, M. J.; Baud, P., Univ Strasbourg, Inst Phys Globe Strasbourg, Lab Deformat Roches, UMR CNRS 7516,EOST, F-67084 Strasbourg, France.}},
DOI = {{10.1016/j.jsg.2013.03.007}},
ISSN = {{0191-8141}},
Keywords = {{Brittle creep; Stress corrosion; Rock deformation; Experimental;
   Long-term strength; Static fatigue}},
Keywords-Plus = {{STRESS-CORROSION; STATIC FATIGUE; ACOUSTIC-EMISSION; MICROCRACK MODEL;
   DAMAGE MECHANICS; WESTERLY GRANITE; TRIAXIAL CREEP; CONFINING PRESSURE;
   TEMPERATURE CREEP; STRAIN RATE}},
Research-Areas = {{Geology}},
Web-of-Science-Categories  = {{Geosciences, Multidisciplinary}},
Author-Email = {{nicolas.brantut@normalesup.org}},
ORCID-Numbers = {{Meredith, Philip/0000-0003-2193-5342}},
Funding-Acknowledgement = {{UK NERC {[}NE/G016909/1]; CNRS PICS grant; ANDRA under the FORPRO
   framework}},
Funding-Text = {{We gratefully acknowledge Neil Hughes, Steve Boon, and John Bowles for
   their assistance and support during experimentation. We have benefited
   from discussions with Andy Bell, Ian Main, Sergio Vinciguerra, and
   Olivier Lengline. We thank Chris Scholz and Yves Gueguen for their
   careful and insightful reviews of the manuscript. N. Brantut and P.
   Meredith were partly funded by UK NERC grant NE/G016909/1
   ``Time-dependent deformation: bridging the strain rate gap in brittle
   rocks{''}. P. Baud and P. Meredith acknowledge the support of CNRS PICS
   grant. Patrick Baud was also partially funded by ANDRA under the FORPRO
   framework. Our thin sections were skillfully prepared by David Mann
   (High Mesa Petrographics).}},
Number-of-Cited-References = {{122}},
Times-Cited = {{78}},
Usage-Count-Last-180-days = {{13}},
Usage-Count-Since-2013 = {{135}},
Journal-ISO = {{J. Struct. Geol.}},
Doc-Delivery-Number = {{178CR}},
Unique-ID = {{ISI:000321422200003}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000326317100007,
Author = {Sangid, Michael D.},
Title = {{The physics of fatigue crack initiation}},
Journal = {{INTERNATIONAL JOURNAL OF FATIGUE}},
Year = {{2013}},
Volume = {{57}},
Number = {{SI}},
Pages = {{58-72}},
Month = {{DEC}},
Note = {{Symposium on Fatique and Microstructure - a Symposium on Recent Advances
   held in Conjunction with the Materials Science and Technology Meeting,
   Columbus, OH, OCT, 2011}},
Abstract = {{The fatigue life of a component can be expressed as the sum of two
   segments of life: (a) the number of loading cycles required to initiate
   a crack and (b) the number of cycles it takes that crack to propagate to
   failure. In this review, the primary emphasis is relating the fatigue
   crack initiation to the microstructure of the material. Many studies
   have focused on this phenomenon over the years and the goal of this
   paper is to put this work in perspective and encourage future work of
   fatigue in polycrystals based on the material's microstructure. In order
   to address fatigue, it is necessary to understand the mechanisms that
   facilitate crack initiation. Slip irreversibilities exist in a material
   and accumulate during fatigue loading. At the defect level,
   irreversibilities are a result of dislocations: annihilating,
   cross-slipping, penetrating precipitates, transmitting through grain
   boundaries, and piling-up. These slip irreversibilities are the early
   signs of damage during cyclic loading. The dislocations subsequently
   form low-energy, stable structures as a means to accommodate the
   irreversible slip processes and increasing dislocation density during
   cyclic forward and reverse loading. The result is strain localizing in a
   small region within the materials, i.e. persistent slip bands and
   dislocation cells/bundles. Strain localization is a precursor to crack
   initiation. This review paper will focus on experimental observations of
   strain localization and the theory and numerical analysis of both slip
   irreversibilities and low energy configuration defect structures. This
   fundamental understanding is necessary to study persistent slip bands in
   FCC metals and alloys including the appropriate characterization,
   theory, and modeling. From this fundamental knowledge both
   micromechanical and crystal plasticity models can be used to predict
   crack initiation, which are also reviewed. Finally, this review ends
   with a discussion of the future of fatigue modeling and experiments. (C)
   2012 Elsevier Ltd. All rights reserved.}},
Publisher = {{ELSEVIER SCI LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, OXON, ENGLAND}},
Type = {{Article; Proceedings Paper}},
Language = {{English}},
Affiliation = {{Sangid, MD (Reprint Author), Purdue Univ, Coll Engn, Sch Aeronaut \& Astronaut, 701 W Stadium Ave, W Lafayette, IN 47907 USA.
   Purdue Univ, Coll Engn, Sch Aeronaut \& Astronaut, W Lafayette, IN 47907 USA.}},
DOI = {{10.1016/j.ijfatigue.2012.10.009}},
ISSN = {{0142-1123}},
EISSN = {{1879-3452}},
Keywords = {{Fatigue; Crack initiation; Microstructure; Slip irreversibility;
   Persistent slip bands}},
Keywords-Plus = {{PERSISTENT SLIP BANDS; COPPER SINGLE-CRYSTALS; LOW-CYCLE-FATIGUE;
   NICKEL-BASE SUPERALLOY; CONSTANT STRAIN AMPLITUDE; ENERGY
   DISLOCATION-STRUCTURES; AUSTENITIC STAINLESS-STEEL; RANGE
   INTERNAL-STRESSES; ATOMIC-FORCE MICROSCOPY; DEFORMED METAL CRYSTALS}},
Research-Areas = {{Engineering; Materials Science}},
Web-of-Science-Categories  = {{Engineering, Mechanical; Materials Science, Multidisciplinary}},
Author-Email = {{msangid@purdue.edu}},
Number-of-Cited-References = {{156}},
Times-Cited = {{74}},
Usage-Count-Last-180-days = {{12}},
Usage-Count-Since-2013 = {{109}},
Journal-ISO = {{Int. J. Fatigue}},
Doc-Delivery-Number = {{243LE}},
Unique-ID = {{ISI:000326317100007}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000322691000004,
Author = {Savija, Branko and Pacheco, Jose and Schlangen, Erik},
Title = {{Lattice modeling of chloride diffusion in sound and cracked concrete}},
Journal = {{CEMENT \& CONCRETE COMPOSITES}},
Year = {{2013}},
Volume = {{42}},
Pages = {{30-40}},
Month = {{SEP}},
Abstract = {{Reinforced concrete structures are frequently exposed to aggressive
   environmental conditions. Most notably, chloride ions from sea water or
   de-icing salts are potentially harmful since they promote corrosion of
   steel reinforcement. Concrete cover of sufficient quality and depth can
   ensure protection of the steel reinforcement. However, it is necessary
   to study the effects of material heterogeneity and cracking on chloride
   ingress in concrete. This is done herein by proposing a
   three-dimensional lattice model capable of simulating chloride transport
   in saturated sound and cracked concrete. Means of computationally
   determining transport properties of individual phases in heterogeneous
   concrete (aggregate, mortar, and interface), knowing the concrete
   composition and its averaged transport properties, are presented and
   discussed. Based on numerical experimentation and available literature,
   a relation between the effective diffusion coefficient of cracked
   lattice elements and the crack width was adopted. The proposed model is
   coupled with a lattice fracture model to enable simulation of chloride
   ingress in cracked concrete. The model was validated. on data from the
   literature, showing good agreement with experimental results. (C) 2013
   Elsevier Ltd. All rights reserved.}},
Publisher = {{ELSEVIER SCI LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, OXON, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Savija, B (Reprint Author), Delft Univ Technol, Stevinweg 1, NL-2628 CN Delft, Netherlands.
   Savija, Branko; Pacheco, Jose; Schlangen, Erik, Delft Univ Technol, NL-2628 CN Delft, Netherlands.}},
DOI = {{10.1016/j.cemconcomp.2013.05.003}},
ISSN = {{0958-9465}},
Keywords = {{Lattice model; Mesoscale; Cracking; Chloride diffusion; Durability}},
Keywords-Plus = {{LOCAL DIFFUSION; MORTAR; PREDICTION; SIMULATION; MIGRATION; DAMAGE}},
Research-Areas = {{Construction \& Building Technology; Materials Science}},
Web-of-Science-Categories  = {{Construction \& Building Technology; Materials Science, Composites}},
Author-Email = {{b.savija@tudelft.nl
   j.pachecofarias@tudelft.nl
   h.e.j.g.schlangen@tudelft.nl}},
ORCID-Numbers = {{Savija, Branko/0000-0003-1299-1449}},
Funding-Acknowledgement = {{Dutch Technology Foundation (STW) {[}10978]}},
Funding-Text = {{Financial support by the Dutch Technology Foundation (STW) for the
   project 10978 - ``Measuring, Modelling, and Monitoring Chloride ingress
   and Corrosion initiation in Cracked Concrete (M3C4){''} is gratefully
   acknowledged. Constructive comments and suggestions of the reviewers are
   appreciated.}},
Number-of-Cited-References = {{35}},
Times-Cited = {{37}},
Usage-Count-Last-180-days = {{5}},
Usage-Count-Since-2013 = {{48}},
Journal-ISO = {{Cem. Concr. Compos.}},
Doc-Delivery-Number = {{195GT}},
Unique-ID = {{ISI:000322691000004}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000324588700002,
Author = {Kaddour, A. S. and Hinton, M. J. and Smith, P. A. and Li, S.},
Title = {{The background to the third world-wide failure exercise}},
Journal = {{JOURNAL OF COMPOSITE MATERIALS}},
Year = {{2013}},
Volume = {{47}},
Number = {{20-21, SI}},
Pages = {{2417-2426}},
Month = {{SEP}},
Abstract = {{The authors have recently completed two world-wide failure exercises,
   which dealt with benchmarking recognised failure criteria under
   two-dimensional and three-dimensional loadings, respectively. A new
   phase, called the third world-wide failure exercise' is currently
   underway to fill some of the major gaps identified in the previous
   activities. The third world-wide failure exercise is concerned with
   highlighting the degree of maturity of the current capabilities of 12
   internationally recognised methods for modelling various aspects of
   damage in composite materials. Such problems include matrix cracks due
   to thermal and mechanical loads; delamination; ply constraint and
   stacking sequence effects; loading and unloading phenomena; failure due
   to stress gradients (in particular the hole size effect). The topics
   addressed within the third world-wide failure exercise represent an
   extremely important and crucial area for advanced modelling and virtual
   testing of composites. The third world-wide failure exercise runs in two
   stages (1) Part A which is devoted to providing full details and a
   comparison between the 12 theories together with their blind'
   predictions, made by their originators, for a challenging set of test
   problems and (2) Part B which is concerned with comparing the
   theoretical predictions with experimental results and assessing the
   accuracy and maturity of the methods. This paper provides details of the
   background to third world-wide failure exercise, the process of
   completing Part A and a summary of key conclusions.}},
Publisher = {{SAGE PUBLICATIONS LTD}},
Address = {{1 OLIVERS YARD, 55 CITY ROAD, LONDON EC1Y 1SP, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Kaddour, AS (Reprint Author), QinetiQ, Ively Rd, Farnborough GU14 0LX, Hants, England.
   Kaddour, A. S., QinetiQ, Farnborough GU14 0LX, Hants, England.
   Hinton, M. J., Natl Composites Ctr, Bristol, Avon, England.
   Smith, P. A., Univ Surrey, Fac Engn \& Phys Sci, Guildford GU2 5XH, Surrey, England.
   Li, S., Univ Nottingham, Fac Engn, Nottingham NG7 2RD, England.}},
DOI = {{10.1177/0021998313499475}},
ISSN = {{0021-9983}},
EISSN = {{1530-793X}},
Keywords = {{Damage; matrix cracking; delamination; bending; open hole; third
   world-wide failure exercise; failure envelope}},
Research-Areas = {{Materials Science}},
Web-of-Science-Categories  = {{Materials Science, Composites}},
Author-Email = {{askaddour@QinetiQ.com}},
Funding-Acknowledgement = {{Royal Society of the United Kingdom}},
Funding-Text = {{The authors thank the participants who took part in this world-wide
   activity for their dedications. One of the authors (Dr Kaddour) thanks
   the Royal Society of the United Kingdom for the award of a Royal Society
   Industry Fellowship, hosted at the University of Surrey (UK).}},
Number-of-Cited-References = {{19}},
Times-Cited = {{33}},
Usage-Count-Last-180-days = {{4}},
Usage-Count-Since-2013 = {{26}},
Journal-ISO = {{J. Compos Mater.}},
Doc-Delivery-Number = {{220MO}},
Unique-ID = {{ISI:000324588700002}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000321408700007,
Author = {Alnaggar, Mohammed and Cusatis, Gianluca and Di Luzio, Giovanni},
Title = {{Lattice Discrete Particle Modeling (LDPM) of Alkali Silica Reaction
   (ASR) deterioration of concrete structures}},
Journal = {{CEMENT \& CONCRETE COMPOSITES}},
Year = {{2013}},
Volume = {{41}},
Pages = {{45-59}},
Month = {{AUG}},
Abstract = {{A large number of structures especially in high humidity environments
   are endangered by Alkali-Silica Reaction (ASR). ASR leads to the
   formation of an expansive gel that imbibes water over time. The gel
   expansion causes cracking and consequent deterioration of concrete
   mechanical behavior in the form of strength and stiffness reduction. In
   the recent past, many research efforts were directed towards evaluation,
   modeling and treatment of ASR effects on structures but a comprehensive
   computational model is still lacking. In this paper, the ASR effect is
   implemented within the framework of the Lattice Discrete Particle Model
   (LDPM), which simulates concrete heterogeneous character at the scale of
   coarse aggregate pieces. The proposed formulation, entitled ASR-LDPM,
   allows precise and unique modeling of volumetric expansion; expansion
   anisotropy under applied load; non-uniform cracking distribution;
   concrete strength and stiffness degradation; alkali ion concentration
   effect; and temperature effects of concrete subjected to ASR. In
   addition, a unique advantage of this formulation is its ability to
   distinguish between the expansion directly related to ASR gel expansion
   and the one associated with cracking. Simulation of experimental data
   gathered from the literature demonstrates the ability of ASR-LDPM to
   predict accurately ASR-induced concrete deterioration. (C) 2013 Elsevier
   Ltd. All rights reserved.}},
Publisher = {{ELSEVIER SCI LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, OXON, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Cusatis, G (Reprint Author), Northwestern Univ, McCormick Sch Engn \& Appl Sci, Tech Bldg Room A125,2145 N Sheridan Rd, Evanston, IL 60208 USA.
   Alnaggar, Mohammed; Cusatis, Gianluca, Northwestern Univ, Dept Civil \& Environm Engn, Evanston, IL 60208 USA.
   Di Luzio, Giovanni, Politecn Milan, Dept Struct Engn DIS, I-20133 Milan, Italy.}},
DOI = {{10.1016/j.cemconcomp.2013.04.015}},
ISSN = {{0958-9465}},
EISSN = {{1873-393X}},
Keywords = {{Alkali silica reaction; Concrete; Lattice model; Particle model;
   Cracking; Deterioration}},
Keywords-Plus = {{REINFORCED-CONCRETE; AGGREGATE REACTION; MECHANICAL-PROPERTIES; FLY-ASH;
   NUMERICAL SIMULATIONS; REACTION-PRODUCTS; KINETIC APPROACH; DAMAGE
   MODEL; EXPANSION; BEHAVIOR}},
Research-Areas = {{Construction \& Building Technology; Materials Science}},
Web-of-Science-Categories  = {{Construction \& Building Technology; Materials Science, Composites}},
Author-Email = {{MohammedAlnaggar2012@u.northwestern.edu
   g-cusatis@northwestern.edu
   diluzio@stru.polimi.it}},
ResearcherID-Numbers = {{Cusatis, Gianluca/G-2539-2011
   }},
ORCID-Numbers = {{DI LUZIO, Giovanni/0000-0003-1971-8445
   Cusatis, Gianluca/0000-0001-7436-3910}},
Funding-Acknowledgement = {{Science \& Technology Directorate, U.S. Department of Homeland Security
   {[}2009-ST-108-001]}},
Funding-Text = {{This material is based upon work supported by the Science \& Technology
   Directorate, U.S. Department of Homeland Security, under Award Number
   2009-ST-108-001. The views and conclusions contained in this document
   are those of the authors and should not be interpreted as necessarily
   representing the official policies, either expressed or implied, of the
   U.S. Department of Homeland Security.}},
Number-of-Cited-References = {{93}},
Times-Cited = {{33}},
Usage-Count-Last-180-days = {{2}},
Usage-Count-Since-2013 = {{30}},
Journal-ISO = {{Cem. Concr. Compos.}},
Doc-Delivery-Number = {{177XM}},
Unique-ID = {{ISI:000321408700007}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000328432500003,
Author = {Kordatos, E. Z. and Dassios, K. G. and Aggelis, D. G. and Matikas, T. E.},
Title = {{Rapid evaluation of the fatigue limit in composites using infrared
   lock-in thermography and acoustic emission}},
Journal = {{MECHANICS RESEARCH COMMUNICATIONS}},
Year = {{2013}},
Volume = {{54}},
Pages = {{14-20}},
Month = {{DEC}},
Abstract = {{Fatigue limit determination via the conventional Wohler-curve method is
   associated with extended experimental times as it requires testing of a
   large number of specimens. The current paper introduces a methodology
   for fast, reliable and experimentally economic determination of the
   fatigue limit in monolithic and composite materials by means of combined
   usage of two nondestructive inspection methods, namely infrared (IR)
   lock-in thermography and acoustic emission (AE). IR thermography, as a
   real-time and non-contact technique, allowed the detection of heat waves
   generated due to thermo-mechanical coupling as well as of the energy
   dissipated intrinsically during dynamic loading of the material. AE, on
   the other hand, was employed to record the transient waves resulting
   from crack propagation events. Aluminum grade 1050 H16 and cross-ply
   SiC/BMAS ceramic matrix composites were subjected to fatigue loading at
   various stress levels and were monitored by an IR camera and AE sensors.
   The fatigue limit of the monolithic material, obtained by the lock-in
   infrared thermography technique and supported by acoustic emission was
   found to be in agreement with measurements obtained by the conventional
   S-N curve method. The fatigue limit of the ceramic matrix composite was
   validated with acoustic emission data. (C) 2013 Elsevier Ltd. All rights
   reserved.}},
Publisher = {{PERGAMON-ELSEVIER SCIENCE LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Matikas, TE (Reprint Author), Univ Ioannina, Dept Mat Sci \& Engn, GR-45110 Ioannina, Greece.
   Kordatos, E. Z.; Dassios, K. G.; Aggelis, D. G.; Matikas, T. E., Univ Ioannina, Dept Mat Sci \& Engn, GR-45110 Ioannina, Greece.
   Aggelis, D. G., Vrije Univ Brussel, Dept Mech Mat \& Construct, B-1050 Brussels, Belgium.}},
DOI = {{10.1016/j.mechrescom.2013.09.005}},
ISSN = {{0093-6413}},
Keywords = {{Fatigue limit; Lock-in thermography; Acoustic emission; CMC}},
Keywords-Plus = {{CERAMIC-MATRIX COMPOSITES; DAMAGE EVALUATION; CONCRETE; STRESS; GLASS;
   FRACTURE; MECHANISMS; BEHAVIOR; METALS}},
Research-Areas = {{Mechanics}},
Web-of-Science-Categories  = {{Mechanics}},
Author-Email = {{matikas@otenet.gr}},
ORCID-Numbers = {{Dassios, Konstantinos/0000-0003-2045-8900
   KORDATOS, EVANGELOS/0000-0002-5448-3883}},
Number-of-Cited-References = {{40}},
Times-Cited = {{32}},
Usage-Count-Last-180-days = {{5}},
Usage-Count-Since-2013 = {{45}},
Journal-ISO = {{Mech. Res. Commun.}},
Doc-Delivery-Number = {{272AK}},
Unique-ID = {{ISI:000328432500003}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000318504500055,
Author = {Wu, Xiang-Fa and Rahman, Arifur and Zhou, Zhengping and Pelot, David D.
   and Sinha-Ray, Suman and Chen, Bin and Payne, Scott and Yarin, Alexander
   L.},
Title = {{Electrospinning core-shell nanofibers for interfacial toughening and
   self-healing of carbon-fiber/epoxy composites}},
Journal = {{JOURNAL OF APPLIED POLYMER SCIENCE}},
Year = {{2013}},
Volume = {{129}},
Number = {{3}},
Pages = {{1383-1393}},
Month = {{AUG 5}},
Abstract = {{This article reports a novel hybrid multiscale carbon-fiber/epoxy
   composite reinforced with self-healing core-shell nanofibers at
   interfaces. The ultrathin self-healing fibers were fabricated by means
   of coelectrospinning, in which liquid dicyclopentadiene (DCPD) as the
   healing agent was enwrapped into polyacrylonitrile (PAN) to form
   core-shell DCPD/PAN nanofibers. These core-shell nanofibers were
   incorporated at interfaces of neighboring carbon-fiber fabrics prior to
   resin infusion and formed into ultrathin self-healing interlayers after
   resin infusion and curing. The core-shell DCPD/PAN fibers are expected
   to function to self-repair the interfacial damages in composite
   laminates, e.g., delamination. Wet layup, followed by vacuum-assisted
   resin transfer molding (VARTM) technique, was used to process the
   proof-of-concept hybrid multiscale self-healing composite. Three-point
   bending test was utilized to evaluate the self-healing effect of the
   core-shell nanofibers on the flexural stiffness of the composite
   laminate after predamage failure. Experimental results indicate that the
   flexural stiffness of such novel self-healing composite after predamage
   failure can be completely recovered by the self-healing nanofiber
   interlayers. Scanning electron microscope (SEM) was utilized for
   fractographical analysis of the failed samples. SEM micrographs clearly
   evidenced the release of healing agent at laminate interfaces and the
   toughening and self-healing mechanisms of the core-shell nanofibers.
   This study expects a family of novel high-strength, lightweight
   structural polymer composites with self-healing function for potential
   use in aerospace and aeronautical structures, sports utilities, etc. (c)
   2012 Wiley Periodicals, Inc. J. Appl. Polym. Sci., 2013}},
Publisher = {{WILEY-BLACKWELL}},
Address = {{111 RIVER ST, HOBOKEN 07030-5774, NJ USA}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Wu, XF (Reprint Author), N Dakota State Univ, Dept Mech Engn, Fargo, ND 58108 USA.
   Wu, Xiang-Fa; Rahman, Arifur; Zhou, Zhengping, N Dakota State Univ, Dept Mech Engn, Fargo, ND 58108 USA.
   Pelot, David D.; Sinha-Ray, Suman; Yarin, Alexander L., Univ Illinois, Dept Mech \& Ind Engn, Chicago, IL 60607 USA.
   Chen, Bin, NASA, Ames Res Ctr, Adv Studies Lab, Moffett Field, CA 94035 USA.
   Chen, Bin, Univ Calif Santa Cruz, Baskin Sch Engn, Santa Cruz, CA 95064 USA.
   Payne, Scott, N Dakota State Univ, Electron Microscopy Ctr, Fargo, ND 58108 USA.}},
DOI = {{10.1002/app.38838}},
ISSN = {{0021-8995}},
Keywords = {{electrospinning; fibers; mechanical properties; nanostructured polymers}},
Keywords-Plus = {{EPOXY COMPOSITE; FATIGUE CRACKS; FRACTURE-TOUGHNESS; POLYMER NANOFIBERS;
   GLASS NANOFIBERS; FIBERS; COATINGS; REPAIR; RESINS; DAMAGE}},
Research-Areas = {{Polymer Science}},
Web-of-Science-Categories  = {{Polymer Science}},
Author-Email = {{xiangfa.wu@ndsu.edu
   ayarin@uic.edu}},
Funding-Acknowledgement = {{NDSU by the ND NASA EPSCoR (NASA) {[}NNX07AK91A, 43500-2490-FAR018640];
   NDSU Development Foundation}},
Funding-Text = {{The financial support of the research at NDSU by the ND NASA EPSCoR
   (NASA Grant \# NNX07AK91A, seed grant: 43500-2490-FAR018640) and NDSU
   Development Foundation (XFW) was gratefully acknowledged. Thanks go to
   Professor Chunwei Sun of the Department of Pharmacy at NDSU for kind
   assistance with the optical microscopy of the core-shell nanofibers.}},
Number-of-Cited-References = {{57}},
Times-Cited = {{32}},
Usage-Count-Last-180-days = {{10}},
Usage-Count-Since-2013 = {{237}},
Journal-ISO = {{J. Appl. Polym. Sci.}},
Doc-Delivery-Number = {{138JJ}},
Unique-ID = {{ISI:000318504500055}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000318579500004,
Author = {Wei, Xiaoding and Phuong Tran and de Vaucorbeil, Alban and Ramaswamy,
   Ravi Bellur and Latourte, Felix and Espinosa, Horacio D.},
Title = {{Three-dimensional numerical modeling of composite panels subjected to
   underwater blast}},
Journal = {{JOURNAL OF THE MECHANICS AND PHYSICS OF SOLIDS}},
Year = {{2013}},
Volume = {{61}},
Number = {{6}},
Pages = {{1319-1336}},
Month = {{JUN}},
Abstract = {{Designing lightweight high-performance materials that can sustain high
   impulsive loadings is of great interest for marine applications. In this
   study, a finite element fluid-structure interaction model was developed
   to understand the deformation and failure mechanisms of both monolithic
   and sandwich composite panels. Fiber (E-glass fiber) and matrix
   (vinylester resin) damage and degradation in individual unidirectional
   composite laminas were modeled using Hashin failure model. The
   delamination between laminas was modeled by a strain-rate sensitive
   cohesive law. In sandwich panels, core compaction (H250 PVC foam) is
   modeled by a crushable foam plasticity model with volumetric hardening
   and strain-rate sensitivity. The model-predicted deformation histories,
   fiber/matrix damage patterns, and inter-lamina delamination, in both
   monolithic and sandwich composite panels, were compared with
   experimental observations. The simulations demonstrated that the
   delamination process is strongly rate dependent, and that Hashin model
   captures the spatial distribution and magnitude of damage to a
   first-order approximation. The model also revealed that the foam plays
   an important role in improving panel performance by mitigating the
   transmitted impulse to the back-side face sheet while maintaining
   overall bending stiffness. (C) 2013 Elsevier Ltd. All rights reserved.}},
Publisher = {{PERGAMON-ELSEVIER SCIENCE LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Espinosa, HD (Reprint Author), Northwestern Univ, Dept Mech Engn, 2145 Sheridan Rd, Evanston, IL 60208 USA.
   Wei, Xiaoding; Phuong Tran; de Vaucorbeil, Alban; Ramaswamy, Ravi Bellur; Latourte, Felix; Espinosa, Horacio D., Northwestern Univ, Dept Mech Engn, Evanston, IL 60208 USA.}},
DOI = {{10.1016/j.jmps.2013.02.007}},
ISSN = {{0022-5096}},
Keywords = {{Finite element analysis; Fluid-structure interaction; Composite failure;
   Underwater blast; De lamination; Foam compaction}},
Keywords-Plus = {{METAL SANDWICH PLATES; FIBER-REINFORCED MATERIALS; DEPENDENT COHESIVE
   ZONE; DYNAMIC-RESPONSE; CRACK-GROWTH; IMPULSIVE LOADS; FAILURE;
   BEHAVIOR; DEFORMATION; PERFORMANCE}},
Research-Areas = {{Materials Science; Mechanics; Physics}},
Web-of-Science-Categories  = {{Materials Science, Multidisciplinary; Mechanics; Physics, Condensed
   Matter}},
Author-Email = {{espinosa@northwestern.edu}},
ResearcherID-Numbers = {{Espinosa, Horatio/B-6693-2009
   Wei, Xiaoding/A-9952-2011}},
ORCID-Numbers = {{Wei, Xiaoding/0000-0002-5173-4923}},
Funding-Acknowledgement = {{Office of Naval Research (ONR) {[}N00014-08-1-1055]}},
Funding-Text = {{This research was carried out under the financial support of the Office
   of Naval Research (ONR) under grant number N00014-08-1-1055. The support
   and encouragement provided by Dr. Rajapakse through the study is greatly
   appreciated.}},
Number-of-Cited-References = {{60}},
Times-Cited = {{32}},
Usage-Count-Last-180-days = {{3}},
Usage-Count-Since-2013 = {{50}},
Journal-ISO = {{J. Mech. Phys. Solids}},
Doc-Delivery-Number = {{139JR}},
Unique-ID = {{ISI:000318579500004}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000313406700006,
Author = {Lim, M. L. C. and Scully, J. R. and Kelly, R. G.},
Title = {{Intergranular Corrosion Penetration in an Al-Mg Alloy as a Function of
   Electrochemical and Metallurgical Conditions}},
Journal = {{CORROSION}},
Year = {{2013}},
Volume = {{69}},
Number = {{1}},
Month = {{JAN}},
Abstract = {{An experimental and modeling study of factors influencing intergranular
   corrosion (IGC) penetration depth into an Al-Mg alloy, AA5083 (UNS
   A95083), is presented. Potentiostatic tests over a range of potentials
   in 0.6 M sodium chloride (NaCl) solution were conducted on longitudinal
   by long transverse (LT), long transverse by short transverse (ST), and
   longitudinal by short transverse (LS) surfaces of sensitized AA5083. The
   IGC penetration rate was found to depend on applied potential, degree of
   sensitization (DoS), exposure time, and propagation direction relative
   to the rolling direction. Statistical IGC depth distributions were
   analyzed and served as inputs for a phenomenological model to estimate
   IGC damage progression for AA5083 during exposure to 0.6 M NaCl solution
   at pH 8.3. This model was validated by comparing the model predicted and
   experimental depths for the 100 degrees C sensitization condition.
   Extension of this combined experimental and modeling approach to the 80
   degrees C sensitization demonstrated that sensitization temperature is
   another significant factor in IGC penetration depths.}},
Publisher = {{NATL ASSOC CORROSION ENG}},
Address = {{1440 SOUTH CREEK DRIVE, HOUSTON, TX 77084-4906 USA}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Kelly, RG (Reprint Author), Univ Virginia, Ctr Electrochem Sci \& Engn, Dept Mat Sci \& Engn, Charlottesville, VA 22904 USA.
   Lim, M. L. C.; Scully, J. R.; Kelly, R. G., Univ Virginia, Ctr Electrochem Sci \& Engn, Dept Mat Sci \& Engn, Charlottesville, VA 22904 USA.}},
DOI = {{10.5006/0722}},
ISSN = {{0010-9312}},
Keywords = {{AA5083; aluminum-magnesium alloy; intergranular corrosion; modeling;
   sensitization}},
Keywords-Plus = {{SENSITIZED AA5083 AL-4.5MG-1.0MN; STRESS-CORROSION; LOCALIZED CORROSION;
   INTERMETALLIC PHASES; ALUMINUM-ALLOYS; NACL SOLUTION; CRACKING
   SUSCEPTIBILITY; CU ALLOYS; ZN-MG; PRECIPITATION}},
Research-Areas = {{Materials Science; Metallurgy \& Metallurgical Engineering}},
Web-of-Science-Categories  = {{Materials Science, Multidisciplinary; Metallurgy \& Metallurgical
   Engineering}},
Author-Email = {{rgk6y@virginia.edu}},
Funding-Acknowledgement = {{Office of Naval Research {[}N000140810315]}},
Funding-Text = {{This work was funded by the Office of Naval Research Grant N000140810315
   with A. Perez as Scientific Officer. We would like to recognize the
   technical assistance given by W. Adedeji, L. Chen, and S. Jain.}},
Number-of-Cited-References = {{56}},
Times-Cited = {{32}},
Usage-Count-Last-180-days = {{1}},
Usage-Count-Since-2013 = {{55}},
Journal-ISO = {{Corrosion}},
Doc-Delivery-Number = {{069AG}},
Unique-ID = {{ISI:000313406700006}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000317845600002,
Author = {Lian, J. and Sharaf, M. and Archie, F. and Muenstermann, S.},
Title = {{A hybrid approach for modelling of plasticity and failure behaviour of
   advanced high-strength steel sheets}},
Journal = {{INTERNATIONAL JOURNAL OF DAMAGE MECHANICS}},
Year = {{2013}},
Volume = {{22}},
Number = {{2}},
Pages = {{188-218}},
Month = {{MAR}},
Abstract = {{The ductile damage mechanisms dominating in modern high-strength steels
   have emphasised the significance of the onset of damage and the
   subsequent damage evolution in sheet metal forming processes. This paper
   contributes to the modelling of the plasticity and ductile damage
   behaviour of a dual-phase steel sheet by proposing a new damage
   mechanics approach derived from the combination of different types of
   damage models. It addresses the influence of stress state on the
   plasticity behaviour and onset of damage of materials, and quantifies
   the microstructure degradation using a dissipation-energy-based damage
   evolution law. The model is implemented into ABAQUS/Explicit by means of
   a user material subroutine (VUMAT) and applied to the subsequent
   numerical simulations. A hybrid experimental and numerical approach is
   employed to calibrate the material parameters, and the detailed program
   is demonstrated. The calibrated parameters and the model are then
   verified by experiments at different levels, and a good agreement
   between the experimental and numerical results is achieved.}},
Publisher = {{SAGE PUBLICATIONS LTD}},
Address = {{1 OLIVERS YARD, 55 CITY ROAD, LONDON EC1Y 1SP, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Lian, J (Reprint Author), Rhein Westfal TH Aachen, Dept Ferrous Met, Aachen, Germany.
   Lian, J.; Sharaf, M.; Muenstermann, S., Rhein Westfal TH Aachen, Dept Ferrous Met, Aachen, Germany.
   Archie, F., German Univ Cairo, Cairo, Egypt.}},
DOI = {{10.1177/1056789512439319}},
ISSN = {{1056-7895}},
Keywords = {{AHSS; ductile damage and fracture; damage models; crack initiation; FEM
   simulation}},
Keywords-Plus = {{MODIFIED GURSON MODEL; SHEAR MODIFIED GURSON; DUCTILE FRACTURE;
   ELLIPSOIDAL CAVITIES; STRESS TRIAXIALITIES; NONSPHERICAL VOIDS;
   APPROXIMATE MODELS; TENSILE SPECIMEN; DAMAGE MECHANICS; YIELD CRITERION}},
Research-Areas = {{Materials Science; Mechanics}},
Web-of-Science-Categories  = {{Materials Science, Multidisciplinary; Mechanics}},
Author-Email = {{junhe.lian@iehk.rwth-aachen.de}},
ResearcherID-Numbers = {{Munstermann, Sebastian/E-5480-2012
   Lian, Junhe/C-5492-2009}},
ORCID-Numbers = {{Munstermann, Sebastian/0000-0002-6251-2429
   Lian, Junhe/0000-0003-0323-3486}},
Funding-Acknowledgement = {{Deutsche Forschungsgemeinschaft (DFG) {[}MU 2977/1-1]}},
Funding-Text = {{The authors also gratefully acknowledge the Deutsche
   Forschungsgemeinschaft (DFG) for providing the financial funding for the
   project `MU 2977/1-1', which formed the basis for the investigations
   detailed in this paper.}},
Number-of-Cited-References = {{56}},
Times-Cited = {{31}},
Usage-Count-Last-180-days = {{1}},
Usage-Count-Since-2013 = {{29}},
Journal-ISO = {{Int. J. Damage Mech.}},
Doc-Delivery-Number = {{129MU}},
Unique-ID = {{ISI:000317845600002}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000314482500022,
Author = {Hin, Ellemieke S. and Wu, Min-Kai and Wesselink, Paul R. and Shemesh,
   Hagay},
Title = {{Effects of Self-Adjusting File, Mtwo, and Pro Taper on the Root Canal
   Wall}},
Journal = {{JOURNAL OF ENDODONTICS}},
Year = {{2013}},
Volume = {{39}},
Number = {{2}},
Pages = {{262-264}},
Month = {{FEB}},
Abstract = {{Introduction: The purpose of this ex vivo study was to observe the
   incidence of cracks in root dentin after root canal preparation with
   hand files, self-adjusting file (SAF), ProTaper, and Mtwo. Methods: One
   hundred extracted mandibular premolars with single canals were randomly
   selected. Two angulated radiographs were taken for each tooth, and the
   width of the canal was measured at 9 mm from the apex. Five groups of 20
   teeth each were comparable in canal width. The control group was left
   unprepared. Four experimental groups were instrumented with hand files,
   ProTaper, Mtwo, and SAF. Roots were then sectioned horizontally and
   observed under a microscope. The presence of dentinal cracks and their
   location were noted. The difference between the experimental groups was
   analyzed with a chi(2) test. Results: No cracks were observed in the
   control group. In the experimental groups, ProTaper, Mtwo, and SAF
   caused cracks in 35\%, 25\%, and 10\% of teeth, respectively. The
   hand-file group did not show any dentinal cracks (P < .0001). ProTaper
   and Mtwo caused more cracks than hand files (P < .05), but SAF did not
   (P > .05). Conclusions: Instrumentation of root canals with SAF, Mtwo,
   and ProTaper could cause damage to root canal dentin. SAF has a tendency
   to cause less dentinal cracks as compared with ProTaper or Mtwo. (J
   Endod 2013;39:262-264)}},
Publisher = {{ELSEVIER SCIENCE INC}},
Address = {{360 PARK AVE SOUTH, NEW YORK, NY 10010-1710 USA}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Shemesh, H (Reprint Author), Univ Amsterdam, Acad Ctr Dent Amsterdam ACTA, Dept Endodontol, Gustav Mahlerlaan 3004, NL-1081 LA Amsterdam, Netherlands.
   Shemesh, Hagay, Univ Amsterdam, Acad Ctr Dent Amsterdam ACTA, Dept Endodontol, NL-1081 LA Amsterdam, Netherlands.
   Shemesh, Hagay, Vrije Univ Amsterdam, NL-1081 LA Amsterdam, Netherlands.}},
DOI = {{10.1016/j.joen.2012.10.020}},
ISSN = {{0099-2399}},
Keywords = {{Crack; dentin; Mtwo; ProTaper; root fracture; SAF}},
Keywords-Plus = {{NITI ROTARY INSTRUMENTS; PART 2; TOMOGRAPHY; FRACTURE; TEETH}},
Research-Areas = {{Dentistry, Oral Surgery \& Medicine}},
Web-of-Science-Categories  = {{Dentistry, Oral Surgery \& Medicine}},
Author-Email = {{hshemesh@acta.nl}},
ResearcherID-Numbers = {{Shemesh, Hagay/L-7793-2017}},
ORCID-Numbers = {{Shemesh, Hagay/0000-0002-4840-048X}},
Number-of-Cited-References = {{21}},
Times-Cited = {{31}},
Usage-Count-Last-180-days = {{0}},
Usage-Count-Since-2013 = {{11}},
Journal-ISO = {{J. Endod.}},
Doc-Delivery-Number = {{083RI}},
Unique-ID = {{ISI:000314482500022}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000329080900007,
Author = {Saafi, Mohamed and Andrew, Kelly and Tang, Pik Leung and McGhon, David
   and Taylor, Steven and Rahman, Mahubur and Yang, Shangtong and Zhou,
   Xiangming},
Title = {{Multifunctional properties of carbon nanotube/fly ash geopolymeric
   nanocomposites}},
Journal = {{CONSTRUCTION AND BUILDING MATERIALS}},
Year = {{2013}},
Volume = {{49}},
Pages = {{46-55}},
Month = {{DEC}},
Abstract = {{Fly ash-based geopolymers are currently being considered as a viable
   replacement to ordinary Portland cement (OPC) due to multifold benefits
   such as cost efficiency, chemical stability, corrosion resistance, rapid
   strength gain rate, low shrinkage and freeze-thaw resistance. However,
   geopolymers tend to be more brittle than OPC and thus unsuitable for
   concrete structures due to safety concerns. Geopolymers with improved
   electrical properties can also be used as self-sensing materials capable
   of detect their own structural damage. Therefore, this paper is aimed at
   investigating the effect of multiwalled carbon nanotubes (MWCNTs) on the
   mechanical and electrical properties of fly ash (FA) geopolymeric
   composites. Geopolymeric matrices containing different MWCNTs
   concentrations (0.0\%, 0.1\%, 0.5\% and 1.0\% by weight) were
   synthesized and their mechanical properties (i.e., flexural strength,
   Young's modulus, flexural toughness and fracture energy), electrical
   conductivity and piezoresistive response were determined. A scanning
   electron microscope (SEM) was employed to evaluate the distribution
   quality of MWCNTs within the matrix and determine their crack-bridging
   mechanism. The experimental results showed that the MWCNTs were
   uniformly distributed within the matrix at 0.1 and 0.5-wt\% and they
   were poorly distributed and severely agglomerated within the matrix at
   1-wt\%. The experimental results also showed that the addition of MWCNTs
   increased the flexural strength, Young's modulus and flexural toughness
   by as much as 160\%, 109\% and 275\%, respectively. The MWCNTs also
   enhanced the fracture energy and increased the electrical conductivity
   by 194\%. The geopolymeric nanocomposites exhibited a piezoresistive
   response with high sensitivity to micro-crack propagation. (C) 2013
   Elsevier Ltd. All rights reserved.}},
Publisher = {{ELSEVIER SCI LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, OXON, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Saafi, M (Reprint Author), Univ Strathclyde, Dept Civil \& Environm Engn, Glasgow G4 0NG, Lanark, Scotland.
   Saafi, Mohamed; Andrew, Kelly; McGhon, David; Taylor, Steven; Rahman, Mahubur; Yang, Shangtong, Univ Strathclyde, Dept Civil \& Environm Engn, Glasgow G4 0NG, Lanark, Scotland.
   Tang, Pik Leung, Agilent Technol, Mobile Measurement Grp, Edinburgh EH12 9DJ, Midlothian, Scotland.
   Zhou, Xiangming, Brunel Univ, Sch Engn, Uxbridge UB8 3PH, Middx, England.}},
DOI = {{10.1016/j.conbuildmat.2013.08.007}},
ISSN = {{0950-0618}},
EISSN = {{1879-0526}},
Keywords = {{Fly ash; Ceopolymer; Carbon nanotubes; Multifunctional nanocomposites}},
Keywords-Plus = {{ELECTRICAL-CONDUCTIVITY; ELEVATED-TEMPERATURES; MECHANICAL-PROPERTIES;
   CEMENT PASTE; COMPOSITES; CONCRETE}},
Research-Areas = {{Construction \& Building Technology; Engineering; Materials Science}},
Web-of-Science-Categories  = {{Construction \& Building Technology; Engineering, Civil; Materials
   Science, Multidisciplinary}},
Author-Email = {{m.bensalem.saafi@strath.ac.uk}},
ORCID-Numbers = {{Zhou, Xiangming/0000-0001-7977-0718}},
Number-of-Cited-References = {{21}},
Times-Cited = {{30}},
Usage-Count-Last-180-days = {{4}},
Usage-Count-Since-2013 = {{38}},
Journal-ISO = {{Constr. Build. Mater.}},
Doc-Delivery-Number = {{281DT}},
Unique-ID = {{ISI:000329080900007}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000325510900016,
Author = {Solis, Mario and Algaba, Mario and Galvin, Pedro},
Title = {{Continuous wavelet analysis of mode shapes differences for damage
   detection}},
Journal = {{MECHANICAL SYSTEMS AND SIGNAL PROCESSING}},
Year = {{2013}},
Volume = {{40}},
Number = {{2}},
Pages = {{645-666}},
Month = {{NOV}},
Abstract = {{This paper presents a new damage detection methodology for beams. It
   applies wavelet analysis to locate the damage from changes in the mode
   shapes (geometric based analysis). The proposed methodology requires the
   mode shapes of a reference undamaged state as well as those of the
   potentially damaged one. Once obtained, a continuous wavelet transform
   is applied to the difference of the mode shape vectors to obtain
   information of the changes in each of them. Finally, the results for
   each mode are added up to compute an overall result along the structure.
   For the addition, the wavelet coefficients of each mode are weighted
   according to the corresponding variation of the natural frequency. By
   doing so, emphasis is given on those modes that are more likely to be
   affected by damage. On the other hand, mode shapes that have not changed
   their natural frequencies are disregarded. The proposed methodology also
   includes mathematical techniques to avoid wavelet transform edge effect,
   experimental noise reduction in mode shapes and creation of new virtual
   measuring points. It has been validated by experimental analysis of
   steel beams with cracks of different sizes and at different locations.
   The results show that the method is sensitive to little damage. The
   paper analyses the severity threshold of damage and the required number
   of sensors to obtain successful results. (C) 2013 Elsevier Ltd. All
   rights reserved.}},
Publisher = {{ACADEMIC PRESS LTD- ELSEVIER SCIENCE LTD}},
Address = {{24-28 OVAL RD, LONDON NW1 7DX, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Galvin, P (Reprint Author), Univ Seville, Escuela Tecn Super Ingn, Camino Descubrimientos, Seville 41092, Spain.
   Solis, Mario; Algaba, Mario; Galvin, Pedro, Univ Seville, Escuela Tecn Super Ingn, Seville 41092, Spain.}},
DOI = {{10.1016/j.ymssp.2013.06.006}},
ISSN = {{0888-3270}},
Keywords = {{Damage detection; Wavelet analysis; Structural health monitoring; Modal
   analysis; Beams}},
Keywords-Plus = {{STOCHASTIC SUBSPACE IDENTIFICATION; SIMPLY-SUPPORTED BEAMS; CRACK
   DETECTION; TRANSFORM; LOCATION; BASES}},
Research-Areas = {{Engineering}},
Web-of-Science-Categories  = {{Engineering, Mechanical}},
Author-Email = {{pedrogalvin@us.es}},
ResearcherID-Numbers = {{Solis, Mario/J-6145-2013
   Galvin, Pedro/E-6293-2010}},
ORCID-Numbers = {{Solis, Mario/0000-0002-4482-0145
   Galvin, Pedro/0000-0001-8981-1413}},
Funding-Acknowledgement = {{Spanish Ministry of Economy and Competitiveness (Ministerio de Economia
   y Competitividad) {[}BIA2010-14843]}},
Funding-Text = {{This research was funded by the Spanish Ministry of Economy and
   Competitiveness (Ministerio de Economia y Competitividad) through
   research project BIA2010-14843. Financial support is gratefully
   acknowledged.}},
Number-of-Cited-References = {{49}},
Times-Cited = {{29}},
Usage-Count-Last-180-days = {{1}},
Usage-Count-Since-2013 = {{35}},
Journal-ISO = {{Mech. Syst. Signal Proc.}},
Doc-Delivery-Number = {{232RE}},
Unique-ID = {{ISI:000325510900016}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000320294800002,
Author = {Bogdanovich, Alexander E. and Karahan, Mehmet and Lomov, Stepan V. and
   Verpoest, Ignaas},
Title = {{Quasi-static tensile behavior and damage of carbon/epoxy composite
   reinforced with 3D non-crimp orthogonal woven fabric}},
Journal = {{MECHANICS OF MATERIALS}},
Year = {{2013}},
Volume = {{62}},
Pages = {{14-31}},
Month = {{AUG 1}},
Abstract = {{This paper presents a comprehensive experimental study and detailed
   mechanistic interpretations of the tensile behavior of one
   representative 3D non-crimp orthogonal woven (3DNCOW) carbon/epoxy
   composite. The composite is tested under uniaxial in-plane tensile
   loading in the warp, fill and +/- 45 degrees bias directions. An
   ``S-shape{''} nonlinearity observed in the stress-strain curves is
   explained by the concurrent contributions of inherent carbon fiber
   stiffening ({''}non-Hookean behavior{''}), fiber straightening, and
   gradual damage accumulation. Several approaches to the determination of
   a single-value Young's modulus from a significantly nonlinear
   stress-strain curve are discussed and the best approach recommended.
   Also, issues related to the experimental determination of effective
   Poisson's ratios for this class of composites are discussed, and their
   possible resolution suggested. The observed experimental values of the
   warp- and fill-directional tensile strengths are much higher than those
   typically obtained for 3D interlock weave carbon/epoxy composites while
   the nonlinear material behavior observed for the +/- 45
   degrees-directional tensile loading is in a qualitative agreement with
   the earlier results for other textile composites. Results of the damage
   initiation and progression, monitoried by means of acoustic emission,
   full-field strain optical measurements, X-rays and optical microscopy,
   are illustrated and discussed in detail. The damage modes at different
   stages of the increasing tensile loading are analyzed, and the principal
   progressive damage mechanisms identified, including the characteristic
   crack patterns developed at each damage stage. It is concluded that
   significant damage initiation of the present material occurs in the same
   strain range as in traditional cross-ply laminates, while respective
   strain range for other previously studied carbon/epoxy textile
   composites is significantly lower. Overall the revealed advantages in
   stiffness, strength and progressive damage behavior of the studied
   composite are mainly attributed to the absence of crimp and only minimal
   fiber waviness in the reinforcing 3DNCOW preform. C) 2013 Elsevier Ltd.
   All rights reserved.}},
Publisher = {{ELSEVIER SCIENCE BV}},
Address = {{PO BOX 211, 1000 AE AMSTERDAM, NETHERLANDS}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Lomov, SV (Reprint Author), Katholieke Univ Leuven, Dept Met \& Mat Engn, Kasteelpk Arenberg 44, B-3001 Louvain, Belgium.
   Karahan, Mehmet; Lomov, Stepan V.; Verpoest, Ignaas, Katholieke Univ Leuven, Dept Met \& Mat Engn, B-3001 Louvain, Belgium.
   Bogdanovich, Alexander E., N Carolina State Univ, Dept Text Engn Chem \& Sci, Raleigh, NC 27695 USA.
   Karahan, Mehmet, Uludag Univ, Vocat Sch Tech Sci, Gorukle, Bursa, Turkey.}},
DOI = {{10.1016/j.mechmat.2013.03.005}},
ISSN = {{0167-6636}},
Keywords = {{Mechanical properties; 3D woven composite; Tensile loading; Elastic
   properties; Strength; Damage initiation and development}},
Keywords-Plus = {{FAILURE; PREFORMS; WEAVE; SHEAR}},
Research-Areas = {{Materials Science; Mechanics}},
Web-of-Science-Categories  = {{Materials Science, Multidisciplinary; Mechanics}},
Author-Email = {{Stepan.Lomov@mtm.kuleuven.be}},
ResearcherID-Numbers = {{Lomov, Stepan/C-2366-2014}},
ORCID-Numbers = {{Lomov, Stepan/0000-0002-8194-4913}},
Funding-Acknowledgement = {{Tubitak scholarship {[}2219]; KU}},
Funding-Text = {{The research visit of Dr. M. Karahan to K.U. Leuven has been funded by a
   Tubitak scholarship (program BIDEB 2219) and supported by KU. Leuven.
   The help of Mr. Bart Pelgrims and Mr. Kris Van de Staye (Department MTM,
   K.U. Leuven) is gratefully acknowledged. The authors are thankful to Dr.
   Dmitri Mungalov, Mr. Ryan Boyle and Mr. Casey Brown (3TEX) for producing
   experimental fabric preforms and composite samples for this study and to
   Dr. Keith Sharp (3TEX) for assistance with proofreading the text.}},
Number-of-Cited-References = {{37}},
Times-Cited = {{28}},
Usage-Count-Last-180-days = {{0}},
Usage-Count-Since-2013 = {{72}},
Journal-ISO = {{Mech. Mater.}},
Doc-Delivery-Number = {{162VT}},
Unique-ID = {{ISI:000320294800002}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000315550700024,
Author = {Hojjati-Talemi, Reza and Wahab, Magd Abdel},
Title = {{Fretting fatigue crack initiation lifetime predictor tool: Using damage
   mechanics approach}},
Journal = {{TRIBOLOGY INTERNATIONAL}},
Year = {{2013}},
Volume = {{60}},
Pages = {{176-186}},
Month = {{APR}},
Abstract = {{Fretting fatigue is a combination of two complex mechanical phenomena.
   Fretting appears between components that are subjected to small relative
   oscillatory motions. Once these connected components undergo cyclic
   fatigue load, fretting fatigue occurs. In general, fretting fatigue
   failure process can be divided into two main portions, namely crack
   initiation and crack propagation. Fretting fatigue crack initiation
   characteristics are very difficult to detect because damages such as
   micro-cracks are always hidden between two contact surfaces.
   In this paper Continuum Damage Mechanics (CDM) approach in conjunction
   with Finite Element Analyses (FEA) is used to find a predictor tool for
   fretting fatigue crack initiation lifetime. For this purpose an
   uncoupled damage evolution law is developed to model fretting fatigue
   crack initiation lifetime at various fretting condition such as contact
   geometry, axial stress, normal load and tangential load. The predicted
   results are validated with published experimental data from literature.
   (C) 2012 Elsevier Ltd. All rights reserved.}},
Publisher = {{ELSEVIER SCI LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, OXON, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Hojjati-Talemi, R (Reprint Author), Technol Pk Zwijnaarde 903, B-9052 Ghent, Belgium.
   Hojjati-Talemi, Reza; Wahab, Magd Abdel, Univ Ghent, Fac Engn \& Architecture, Dept Mech Construct \& Prod, B-9000 Ghent, Belgium.}},
DOI = {{10.1016/j.triboint.2012.10.028}},
ISSN = {{0301-679X}},
Keywords = {{Fretting fatigue; Crack initiation lifetime; Damage mechanics; Stress
   triaxiality}},
Keywords-Plus = {{FINITE-ELEMENT; CRITICAL-PLANE; BEHAVIOR; TI-6AL-4V}},
Research-Areas = {{Engineering}},
Web-of-Science-Categories  = {{Engineering, Mechanical}},
Author-Email = {{Reza.HojjatiTalemi@UGent.be}},
ResearcherID-Numbers = {{Abdel Wahab, Magd/K-4296-2015
   }},
ORCID-Numbers = {{Abdel Wahab, Magd/0000-0002-3610-865X}},
Funding-Acknowledgement = {{Ghent University {[}BOF 01N02410]}},
Funding-Text = {{The authors wish to thank the Ghent University for the financial support
   received by the Special Funding of Ghent University, Bijzonder
   Onderzoeksfonds (BOF), in the framework of project (BOF 01N02410).}},
Number-of-Cited-References = {{33}},
Times-Cited = {{28}},
Usage-Count-Last-180-days = {{2}},
Usage-Count-Since-2013 = {{31}},
Journal-ISO = {{Tribol. Int.}},
Doc-Delivery-Number = {{098LL}},
Unique-ID = {{ISI:000315550700024}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000315748100045,
Author = {Pang, J. C. and Li, S. X. and Wang, Z. G. and Zhang, Z. F.},
Title = {{General relation between tensile strength and fatigue strength of
   metallic materials}},
Journal = {{MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES
   MICROSTRUCTURE AND PROCESSING}},
Year = {{2013}},
Volume = {{564}},
Pages = {{331-341}},
Month = {{MAR 1}},
Abstract = {{With the development of high-strength materials, the existing fatigue
   strength formulae cannot satisfactorily describe the relation between
   fatigue strength sigma(w) and tensile strength sigma(b) of metallic
   materials with a wide range of strength. For a simple but more precise
   prediction, the tensile and fatigue properties of SAE 4340 steel with
   the tensile strengths ranging from 1290 MPa to 2130 MPa obtained in
   virtue of different tempering temperatures were studied in this paper.
   Based on the experimental results of SAE 4340 steel and numerous other
   data available (conventional and newly developed materials), through
   introducing a sensitive factor of defects P, a new universal fatigue
   strength formula sigma(w)=sigma(b)(C-P.sigma(b)) was established for the
   first time. Combining the variation tendency of fatigue crack initiation
   sites and the competition of defects, the fatigue damage mechanisms
   associated with different tensile strengths and cracking sites are
   explained well. The decrease in the fatigue strength at high-strength
   level can be explained by fracture mechanics and attributed to the
   transition of fatigue cracking sites from surface to the inner
   inclusions, resulting in the maximum fatigue strength sigma(max)(w) at
   an appropriate tensile strength level. Therefore, the universal fatigue
   strength formula cannot only explain why many metallic materials with
   excessively high strength do not display high fatigue strength, but also
   provide a new clue for designing the materials or eliminating the
   processing defects of the materials. (c) 2012 Elsevier B.V. All rights
   reserved.}},
Publisher = {{ELSEVIER SCIENCE SA}},
Address = {{PO BOX 564, 1001 LAUSANNE, SWITZERLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Zhang, ZF (Reprint Author), Chinese Acad Sci, Shenyang Natl Lab Mat Sci, Inst Met Res, 72 Wenhua Rd, Shenyang 110016, Peoples R China.
   Pang, J. C.; Li, S. X.; Wang, Z. G.; Zhang, Z. F., Chinese Acad Sci, Shenyang Natl Lab Mat Sci, Inst Met Res, Shenyang 110016, Peoples R China.}},
DOI = {{10.1016/j.msea.2012.11.103}},
ISSN = {{0921-5093}},
EISSN = {{1873-4936}},
Keywords = {{High-strength materials; Tensile strength; Fatigue strength; Fatigue
   crack initiation site; Fatigue damage mechanism}},
Keywords-Plus = {{HIGH-CYCLE FATIGUE; SEVERE PLASTIC-DEFORMATION; INCLUSION SIZE; BEARING
   STEEL; ULTRAHIGH STRENGTH; GIGACYCLE FATIGUE; CARBON-STEELS; BEHAVIOR;
   REGIME; CU}},
Research-Areas = {{Science \& Technology - Other Topics; Materials Science; Metallurgy \&
   Metallurgical Engineering}},
Web-of-Science-Categories  = {{Nanoscience \& Nanotechnology; Materials Science, Multidisciplinary;
   Metallurgy \& Metallurgical Engineering}},
Author-Email = {{zhfzhang@imr.ac.cn}},
ResearcherID-Numbers = {{Pang, Jian Chao/E-7435-2013
   Zhang, Zhefeng/A-9732-2010
   Zhang Group, SPD/C-6497-2014
   ZZF, Fatigue/C-7064-2014}},
Funding-Acknowledgement = {{National Natural Science Foundation of China (NSFC) {[}50625103,
   50890173, 50931005]; National Basic Research Program of China
   {[}2012CB631006]}},
Funding-Text = {{The authors would like to thank Mrs. C. L. Dai and Dr. H. F. Zou for
   their helps of the SEM and EBSD observations. This work is supported by
   National Natural Science Foundation of China (NSFC) under Grant Nos.
   50625103, 50890173, 50931005 and the National Basic Research Program of
   China under grant No. 2012CB631006.}},
Number-of-Cited-References = {{50}},
Times-Cited = {{28}},
Usage-Count-Last-180-days = {{7}},
Usage-Count-Since-2013 = {{71}},
Journal-ISO = {{Mater. Sci. Eng. A-Struct. Mater. Prop. Microstruct. Process.}},
Doc-Delivery-Number = {{101AR}},
Unique-ID = {{ISI:000315748100045}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000317161800023,
Author = {Chowdhury, Piyas B. and Sehitoglu, Huseyin and Rateick, Richard G. and
   Maier, Hans J.},
Title = {{Modeling fatigue crack growth resistance of nanocrystalline alloys}},
Journal = {{ACTA MATERIALIA}},
Year = {{2013}},
Volume = {{61}},
Number = {{7}},
Pages = {{2531-2547}},
Month = {{APR}},
Abstract = {{The description of fatigue crack growth in metals has remained an
   empirical field. To address the physical processes contributing to crack
   advance a model for fatigue crack growth (FCG) has been developed
   utilizing a combined atomistic-continuum approach. In particular, the
   model addresses the important topic of the role of nanoscale coherent
   twin boundaries (CTB) on FCG. We make the central observation that FCG
   is governed by the dislocation glide resistance and the irreversibility
   of crack tip displacement, both influenced by the presence of CTBs. The
   energy barriers for dislocation slip under cyclical conditions are
   calculated as the glide dislocation approaches a twin boundary and
   reacts with the CTB. The atomistically calculated energy barriers
   provide input to a mechanics model for dislocations gliding in a forward
   and reverse manner. This approach allows the irreversibility of
   displacement at the crack tip, defined as the difference between forward
   and reverse flow, to be determined. The simulation results demonstrate
   that for both refinement of twin thickness and a decrease in crack tip
   to twin spacing FCG resistance improves, in agreement with recent
   experimental findings reported in the literature. (C) 2013 Acta
   Materialia Inc. Published by Elsevier Ltd. All rights reserved.}},
Publisher = {{PERGAMON-ELSEVIER SCIENCE LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Sehitoglu, H (Reprint Author), Univ Illinois, Dept Mech Sci \& Engn, 1206 W Green St, Urbana, IL 61801 USA.
   Chowdhury, Piyas B.; Sehitoglu, Huseyin, Univ Illinois, Dept Mech Sci \& Engn, Urbana, IL 61801 USA.
   Rateick, Richard G., Honeywell Aerosp, South Bend, IN 46628 USA.
   Maier, Hans J., Univ Hannover, Inst Werkstoffkunde Mat Sci, D-30823 Garbsen, Germany.}},
DOI = {{10.1016/j.actamat.2013.01.030}},
ISSN = {{1359-6454}},
EISSN = {{1873-2453}},
Keywords = {{Fatigue; Nanocrystalline; Nickel; Damage tolerance; Coherent twin}},
Keywords-Plus = {{COHERENT TWIN BOUNDARIES; CENTERED-CUBIC METALS; MOLECULAR-DYNAMICS;
   RATE SENSITIVITY; ULTRAHIGH STRENGTH; FLOW-STRESS; STRAIN-RATE;
   DEFORMATION; SLIP; DUCTILITY}},
Research-Areas = {{Materials Science; Metallurgy \& Metallurgical Engineering}},
Web-of-Science-Categories  = {{Materials Science, Multidisciplinary; Metallurgy \& Metallurgical
   Engineering}},
Author-Email = {{huseyin@illinois.edu}},
ORCID-Numbers = {{Chowdhury, Piyas/0000-0002-3120-7018}},
Funding-Acknowledgement = {{Honeywell Aerospace Corporation}},
Funding-Text = {{Support for this work was provided primarily by Honeywell Aerospace
   Corporation. We acknowledge the use of the parallel computing resource,
   the Taub cluster, at the University of Illinois.}},
Number-of-Cited-References = {{52}},
Times-Cited = {{27}},
Usage-Count-Last-180-days = {{2}},
Usage-Count-Since-2013 = {{62}},
Journal-ISO = {{Acta Mater.}},
Doc-Delivery-Number = {{120HQ}},
Unique-ID = {{ISI:000317161800023}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000330488800027,
Author = {Papakonstantinou, K. G. and Shinozuka, M.},
Title = {{Probabilistic model for steel corrosion in reinforced concrete
   structures of large dimensions considering crack effects}},
Journal = {{ENGINEERING STRUCTURES}},
Year = {{2013}},
Volume = {{57}},
Pages = {{306-326}},
Month = {{DEC}},
Abstract = {{A probabilistic model for chloride induced corrosion of the reinforcing
   steel in concrete structures is presented in this work. The main purpose
   of this model is to simulate the complex phenomena involved in a
   detailed yet simple way, appropriate for implementation on large-scale,
   real structures. Addressing this problem a time-dependent model is
   developed that can simulate all stages of reinforced concrete corrosion,
   i.e. corrosion initiation, crack initiation and propagation. The
   novelties of the formulation include a new empirical model for the crack
   propagation stage, which combines corrosion crack width with steel-bar
   cross sectional loss, based on published experimental results, and the
   dynamic influence of propagating cracks on the corrosion mechanism.
   Probabilistic concepts are also employed due to numerous sources of
   uncertainty in the degradation model and the extent of damage is
   quantified by considering the spatial variability of the various
   parameters. Probability density functions for certain variables and
   random model parts are suggested as well. A numerical application and a
   critical discussion are presented at the end. Finally, due to the
   variety of covered topics and the extensive reference list, the paper
   can also serve a secondary purpose as a state-of-the-art review source.
   (C) 2013 Elsevier Ltd. All rights reserved.}},
Publisher = {{ELSEVIER SCI LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, OXON, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Papakonstantinou, KG (Reprint Author), Univ Calif Irvine, Dept Civil \& Environm Engn, Irvine, CA 92717 USA.
   Papakonstantinou, K. G.; Shinozuka, M., Univ Calif Irvine, Dept Civil \& Environm Engn, Irvine, CA 92717 USA.}},
DOI = {{10.1016/j.engstruct.2013.06.038}},
ISSN = {{0141-0296}},
EISSN = {{1873-7323}},
Keywords = {{Chloride induced steel corrosion in concrete; Corrosion initiation;
   Crack initiation and propagation; Crack influence; Extent of damage;
   Stochastic fields}},
Keywords-Plus = {{CHLORIDE-INDUCED CORROSION; INDUCED COVER CRACKING; RC STRUCTURES;
   SERVICE LIFE; MARINE-ENVIRONMENT; CONTAMINATED CONCRETE;
   RELIABILITY-ANALYSIS; STOCHASTIC-PROCESSES; PITTING CORROSION; THRESHOLD
   LEVEL}},
Research-Areas = {{Engineering}},
Web-of-Science-Categories  = {{Engineering, Civil}},
Author-Email = {{kpapakon@uci.edu}},
Funding-Acknowledgement = {{National Science Foundation {[}CMMI-1233714]}},
Funding-Text = {{The work reported in this paper has been partially supported by the
   National Science Foundation under Grant No. CMMI-1233714. This support
   is gratefully acknowledged. The authors would also like to thank Dr.
   Seung Jun Kwon for providing some data for this work and for fruitful
   scientific discussions.}},
Number-of-Cited-References = {{149}},
Times-Cited = {{26}},
Usage-Count-Last-180-days = {{3}},
Usage-Count-Since-2013 = {{42}},
Journal-ISO = {{Eng. Struct.}},
Doc-Delivery-Number = {{300UF}},
Unique-ID = {{ISI:000330488800027}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000322059500007,
Author = {Darabi, Masoud K. and Abu Al-Rub, Rashid K. and Masad, Eyad A. and
   Little, Dallas N.},
Title = {{Constitutive modeling of fatigue damage response of asphalt concrete
   materials with consideration of micro-damage healing}},
Journal = {{INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES}},
Year = {{2013}},
Volume = {{50}},
Number = {{19}},
Pages = {{2901-2913}},
Month = {{SEP}},
Abstract = {{A continuum mechanics-based viscodamage (VD) constitutive relationship
   is proposed to model fatigue damage of asphalt concrete. The form for
   the evolution of the viscodamage function is postulated based on the
   damage density which was determined from uniaxial constant strain rate
   tests that were performed at different strain rates. The proposed
   viscodamage model is coupled with Schapery's nonlinear viscoelastic
   (VE), Perzyna's viscoplastic (VP), and micro-damage healing (H) models
   to simulate the nonlinear mechanical response of asphalt concrete during
   fatigue. Numerical algorithms are implemented in the finite element code
   Abaqus via the user material subroutine UMAT. The proposed model is
   validated against extensive experimental data including constant strain
   rate, cyclic displacement controlled, and cyclic stress controlled tests
   over a range of temperatures, strain rates, loading frequencies, and
   stress/strain levels/amplitudes. The model predictions show that the
   VE-VP-VD-H model is capable of predicting the fatigue damage response of
   asphalt concrete subjected to different loading conditions. The results
   demonstrate that micro-damage healing occurs not only during the rest
   period, but also during the cyclic strain controlled tests even in the
   absence of the resting time. (c) 2013 Elsevier Ltd. All rights reserved.}},
Publisher = {{PERGAMON-ELSEVIER SCIENCE LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Abu Al-Rub, RK (Reprint Author), Masdar Inst Sci \& Technol, Abu Dhabi, U Arab Emirates.
   Darabi, Masoud K.; Masad, Eyad A.; Little, Dallas N., Texas A\&M Univ, Zachry Dept Civil Engn, College Stn, TX 77843 USA.
   Abu Al-Rub, Rashid K., Masdar Inst Sci \& Technol, Abu Dhabi, U Arab Emirates.
   Masad, Eyad A., Texas A\&M Univ Qatar, Mech Engn Program, Doha, Qatar.}},
DOI = {{10.1016/j.ijsolstr.2013.05.007}},
ISSN = {{0020-7683}},
Keywords = {{Fatigue damage; Micro-damage healing; Viscoelasticity; Viscoplasticity;
   Asphalt concrete}},
Keywords-Plus = {{VISCOPLASTIC MODEL; VISCOELASTIC MEDIA; FINITE-ELEMENT; CRACK
   INITIATION; MIXES; TIME; THERMODYNAMICS; IMPLEMENTATION; DEFORMATION;
   FRAMEWORK}},
Research-Areas = {{Mechanics}},
Web-of-Science-Categories  = {{Mechanics}},
Author-Email = {{rabualrub@masdar.ac.ae}},
Funding-Acknowledgement = {{Asphalt Research Consortium through the US Federal Highway
   Administration; Qatar National Research Fund (QNRF) through the National
   Priority Research Program {[}08-310-2-110]; QNRF}},
Funding-Text = {{The authors acknowledge the financial support provided by the Asphalt
   Research Consortium through the US Federal Highway Administration. R.K.
   Abu Al-Rub and E. Masad also would like to acknowledge the financial
   support provided by Qatar National Research Fund (QNRF) through the
   National Priority Research Program project 08-310-2-110. The QNRF
   funding supported the development of the viscodamage model for
   predicting the fatigue damage in asphalt pavements (Section 4 of the
   paper). Finally, the authors acknowledge Dr. Richard Kim from North
   Carolina State University for providing the ALF experimental data used
   in this study.}},
Number-of-Cited-References = {{51}},
Times-Cited = {{26}},
Usage-Count-Last-180-days = {{9}},
Usage-Count-Since-2013 = {{84}},
Journal-ISO = {{Int. J. Solids Struct.}},
Doc-Delivery-Number = {{186QP}},
Unique-ID = {{ISI:000322059500007}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000322706000023,
Author = {Li Longbiao and Song Yingdong and Sun Youchao},
Title = {{Estimate Interface Shear Stress of Unidirectional C/SiC Ceramic Matrix
   Composites from Hysteresis Loops}},
Journal = {{APPLIED COMPOSITE MATERIALS}},
Year = {{2013}},
Volume = {{20}},
Number = {{4}},
Pages = {{693-707}},
Month = {{AUG}},
Abstract = {{The tensile-tensile fatigue behavior of unidirectional C/SiC ceramic
   matrix composites at room and elevated temperature has been
   investigated. An approach to estimate the interface shear stress of
   ceramic matrix composites under fatigue loading has been developed.
   Based on the damage mechanisms of fiber sliding relative to matrix in
   the interface debonded region upon unloading and subsequent reloading,
   the unloading interface reverse slip length and reloading interface new
   slip length are determined by the fracture mechanics approach. The
   hysteresis loss energy for the strain energy lost per volume during
   corresponding cycle is formulatd in terms of interface shear stress. By
   comparing the experimental hysteresis loss energy with the computational
   values, the interface shear stress of unidirectional C/SiC ceramic
   composites corresponding to different cycles at room and elevated
   temperatures has been predicted.}},
Publisher = {{SPRINGER}},
Address = {{VAN GODEWIJCKSTRAAT 30, 3311 GZ DORDRECHT, NETHERLANDS}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Li, LB (Reprint Author), Nanjing Univ Aeronaut \& Astronaut, Coll Civil Aviat, 29 Yudao St, Nanjing 210016, Peoples R China.
   Li Longbiao; Sun Youchao, Nanjing Univ Aeronaut \& Astronaut, Coll Civil Aviat, Nanjing 210016, Peoples R China.
   Song Yingdong, Nanjing Univ Aeronaut \& Astronaut, Coll Energy \& Power Engn, Nanjing 210016, Peoples R China.}},
DOI = {{10.1007/s10443-012-9297-0}},
ISSN = {{0929-189X}},
Keywords = {{Ceramic matrix composites; C/SiC; Fatigue; Interface shear stress;
   Hysteresis loops; Matrix cracking; Interface debonding}},
Keywords-Plus = {{MECHANICAL HYSTERESIS; OUT TESTS; FATIGUE; BEHAVIOR; FRICTION; CRACKING}},
Research-Areas = {{Materials Science}},
Web-of-Science-Categories  = {{Materials Science, Composites}},
Author-Email = {{llb451@nuaa.edu.cn}},
Funding-Acknowledgement = {{Postdoctoral Science Foundation of China {[}2012M511274]}},
Funding-Text = {{This work is sponsored by the Postdoctoral Science Foundation of China
   (Grant No. 2012M511274).}},
Number-of-Cited-References = {{24}},
Times-Cited = {{26}},
Usage-Count-Last-180-days = {{2}},
Usage-Count-Since-2013 = {{20}},
Journal-ISO = {{Appl. Compos. Mater.}},
Doc-Delivery-Number = {{195MF}},
Unique-ID = {{ISI:000322706000023}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000318532600042,
Author = {Jassim, Z. A. and Ali, N. N. and Mustapha, F. and Jalil, N. A. Abdul},
Title = {{A review on the vibration analysis for a damage occurrence of a
   cantilever beam}},
Journal = {{ENGINEERING FAILURE ANALYSIS}},
Year = {{2013}},
Volume = {{31}},
Pages = {{442-461}},
Month = {{JUL}},
Abstract = {{Identification of defects in structures and its components is a crucial
   aspect in decision making about their repair and total replacement.
   Failure to detect the faults has various consequences, and sometimes may
   lead to a catastrophic failure. The conducted research work reported
   analytical and experimental investigations on the effects of a crack on
   the cantilever steel beam with circular cross section. The objective of
   this review is to quantify and to determine the extent of the damage
   magnitude and the location of the cantilever beams. In analytical study,
   finite element method (FEA) software was used in developing the model.
   The results showed that, by monitoring the change of the natural
   frequency it is a feasible and viable tool to indicate the damage
   occurrence and magnitude. Unlike for small crack depth, the natural
   frequencies are not a good damage detector. Mode shapes indicated good
   sensitivity to detect the damage magnitude for all crack parameters.
   Frequency Reduction Index (FRI) and Modal Assurance Criteria (MAC) were
   found to be in order a feasible tool to find the magnitude of the damage
   in beam structures. While, Coordinate Modal Assurance Criteria (COMAC)
   and Curvature Change Index (CCI) were used to predict the location of
   the crack tested beams and proved to be feasible. (C) 2013 Elsevier Ltd.
   All rights reserved.}},
Publisher = {{PERGAMON-ELSEVIER SCIENCE LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, ENGLAND}},
Type = {{Review}},
Language = {{English}},
Affiliation = {{Ali, NN (Reprint Author), Univ Putra Malaysia, Civil Dept, Serdang 43400, Malaysia.
   Jassim, Z. A.; Jalil, N. A. Abdul, Univ Putra Malaysia, Mech \& Mfg Dept, Serdang 43400, Malaysia.
   Ali, N. N., Univ Putra Malaysia, Civil Dept, Serdang 43400, Malaysia.
   Mustapha, F., Univ Putra Malaysia, Aerosp Dept, Serdang 43400, Malaysia.}},
DOI = {{10.1016/j.engfailanal.2013.02.016}},
ISSN = {{1350-6307}},
Keywords = {{Vibration analysis; Damage detection; Cantilever beam}},
Keywords-Plus = {{CRACK DETECTION; NATURAL FREQUENCIES; FORCED-VIBRATION; MULTIPLE CRACKS;
   FRAME STRUCTURES; ELEMENT-METHOD; MODE SHAPE; IDENTIFICATION; LOCATION;
   SENSITIVITY}},
Research-Areas = {{Engineering; Materials Science}},
Web-of-Science-Categories  = {{Engineering, Mechanical; Materials Science, Characterization \& Testing}},
Author-Email = {{nisreen\_sofo@yahoo.com}},
ORCID-Numbers = {{Mustapha, Faizal/0000-0002-0191-1653}},
Number-of-Cited-References = {{68}},
Times-Cited = {{26}},
Usage-Count-Last-180-days = {{7}},
Usage-Count-Since-2013 = {{66}},
Journal-ISO = {{Eng. Fail. Anal.}},
Doc-Delivery-Number = {{138TJ}},
Unique-ID = {{ISI:000318532600042}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000314872900008,
Author = {Dodson, J. C. and Inman, D. J.},
Title = {{Thermal sensitivity of Lamb waves for structural health monitoring
   applications}},
Journal = {{ULTRASONICS}},
Year = {{2013}},
Volume = {{53}},
Number = {{3}},
Pages = {{677-685}},
Month = {{MAR}},
Abstract = {{One of the drawbacks of the current Lamb wave structural health
   monitoring methods are the false positives due to changing environmental
   conditions such as temperature. To create an environmental insensitive
   damage detection scheme, the physics of thermal effects on Lamb waves
   must be understood. Dispersion and thermal sensitivity curves for an
   isotropic plate with thermal stress and thermally varying elastic
   modulus are presented. The thermal sensitivity of dispersion curves is
   analytically developed and validated by experimental measurements. The
   group velocity thermal sensitivity highlights temperature insensitive
   features at two critical frequencies. The thermal sensitivity gives us
   insight to how temperature affects Lamb wave speeds in different
   frequency ranges and will help those developing structural health
   monitoring algorithms. Published by Elsevier B.V.}},
Publisher = {{ELSEVIER SCIENCE BV}},
Address = {{PO BOX 211, 1000 AE AMSTERDAM, NETHERLANDS}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Dodson, JC (Reprint Author), USAF, Res Lab, Munit Directorate, Fuzes Branch, 306 W Eglin Blvd,Bldg 432, Eglin AFB, FL 32542 USA.
   Dodson, J. C., USAF, Res Lab, Munit Directorate, Fuzes Branch, Eglin AFB, FL 32542 USA.
   Inman, D. J., Univ Michigan, Dept Aerosp Engn, Ann Arbor, MI 48109 USA.}},
DOI = {{10.1016/j.ultras.2012.10.007}},
ISSN = {{0041-624X}},
Keywords = {{Structural health monitoring; Guided waves; Lamb waves; Thermal
   variation}},
Keywords-Plus = {{ULTRASONIC GUIDED-WAVES; TEMPERATURE STABILITY; SYSTEMS; PROPAGATION;
   SENSORS; CRACK}},
Research-Areas = {{Acoustics; Radiology, Nuclear Medicine \& Medical Imaging}},
Web-of-Science-Categories  = {{Acoustics; Radiology, Nuclear Medicine \& Medical Imaging}},
Author-Email = {{jacob.dodson@eglin.af.mil}},
Funding-Acknowledgement = {{Department of Defense Science, Mathematics, And Research for
   Transformation (SMART) Scholarship for Service program; AFOSR
   {[}FA9550-09-1-0686]}},
Funding-Text = {{J. Dodson would like the acknowledge support from the Department of
   Defense Science, Mathematics, And Research for Transformation (SMART)
   Scholarship for Service program. All research was conducted at the
   Center for Intelligent Material Systems and Structures located at
   Virginia Polytechnic Institute and State University while J. Dodson was
   pursing his graduate degree. The authors also gratefully acknowledge the
   support of AFOSR Grant No. FA9550-09-1-0686 under the guidance of Dr.
   David Stargel.}},
Number-of-Cited-References = {{35}},
Times-Cited = {{26}},
Usage-Count-Last-180-days = {{3}},
Usage-Count-Since-2013 = {{26}},
Journal-ISO = {{Ultrasonics}},
Doc-Delivery-Number = {{088YD}},
Unique-ID = {{ISI:000314872900008}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000323489700006,
Author = {Farhidzadeh, Alireza and Salamone, Salvatore and Singla, Puneet},
Title = {{A probabilistic approach for damage identification and crack mode
   classification in reinforced concrete structures}},
Journal = {{JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES}},
Year = {{2013}},
Volume = {{24}},
Number = {{14}},
Pages = {{1722-1735}},
Month = {{SEP}},
Abstract = {{Reinforced concrete is subjected to deterioration due to aging,
   increased load, and natural hazards. To minimize the maintenance costs
   and to increase the operation lifetime, researchers and practitioners
   are increasingly interested in improving current nondestructive
   evaluation technologies or building advanced structural health
   monitoring strategies. Acoustic emission methods offer an attractive
   solution for nondestructive evaluation/structural health monitoring of
   reinforced concrete structures. In particular, monitoring the
   development of cracks is of large interest because their properties
   reflect not only the condition of concrete as material but also the
   condition of the entire system at structural level. This article
   presents a new probabilistic approach based on Gaussian mixture modeling
   of acoustic emission to classify crack modes in reinforced concrete
   structures. Experimental results obtained in a full-scale reinforced
   concrete shear wall subjected to reversed cyclic loading are used to
   demonstrate and validate the proposed approach.}},
Publisher = {{SAGE PUBLICATIONS LTD}},
Address = {{1 OLIVERS YARD, 55 CITY ROAD, LONDON EC1Y 1SP, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Salamone, S (Reprint Author), SUNY Buffalo, SSRL, Dept Civil Struct \& Environm Engn, 212 Ketter Hall, Buffalo, NY 14260 USA.
   Farhidzadeh, Alireza; Salamone, Salvatore, SUNY Buffalo, SSRL, Dept Civil Struct \& Environm Engn, Buffalo, NY 14260 USA.
   Singla, Puneet, SUNY Buffalo, LAIRS, Dept Mech \& Aerosp Engn, Buffalo, NY 14260 USA.}},
DOI = {{10.1177/1045389X13484101}},
ISSN = {{1045-389X}},
EISSN = {{1530-8138}},
Keywords = {{Acoustic emission; damage identification; Gaussian mixture modeling;
   crack classification; reinforced concrete; cluster analysis}},
Keywords-Plus = {{GAUSSIAN MIXTURE-MODELS; MOMENT TENSOR ANALYSIS; ACOUSTIC-EMISSION;
   FRACTURE PROCESS; TIME; FEATURES; BEAMS}},
Research-Areas = {{Materials Science}},
Web-of-Science-Categories  = {{Materials Science, Multidisciplinary}},
Author-Email = {{ssalamon@buffalo.edu}},
ResearcherID-Numbers = {{Singla, Puneet/D-3642-2012}},
ORCID-Numbers = {{Singla, Puneet/0000-0002-2441-2531}},
Funding-Acknowledgement = {{National Science Foundation (NSF) {[}CMMI-0829978]}},
Funding-Text = {{The authors acknowledge the National Science Foundation (NSF) for
   providing the financial support under Grant No. CMMI-0829978. The
   experiments presented herein could not have been completed without
   contributions from Prof. Whittaker, chair of the department, and the
   staff of the Structural Engineering and Earthquake Simulation Laboratory
   (SEESL) of the State University of New York at Buffalo.}},
Number-of-Cited-References = {{48}},
Times-Cited = {{25}},
Usage-Count-Last-180-days = {{5}},
Usage-Count-Since-2013 = {{40}},
Journal-ISO = {{J. Intell. Mater. Syst. Struct.}},
Doc-Delivery-Number = {{206BC}},
Unique-ID = {{ISI:000323489700006}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000318583100002,
Author = {Almusallam, Tarek H. and Siddiqui, Nadeem A. and Iqbal, Rizwan A. and
   Abbas, Husain},
Title = {{Response of hybrid-fiber reinforced concrete slabs to hard projectile
   impact}},
Journal = {{INTERNATIONAL JOURNAL OF IMPACT ENGINEERING}},
Year = {{2013}},
Volume = {{58}},
Pages = {{17-30}},
Month = {{AUG}},
Abstract = {{In the present study, the effectiveness of hybrid-fibers (a combination
   of steel and plastic fibers) in improving the impact resistance of slabs
   was studied through a detailed experimental program. A total of 54
   hybrid-fiber reinforced slabs were cast in the two groups; each group
   containing 27 slabs. The specimens of the first group were cast using
   normal strength concrete, whereas specimens of second group were cast
   using high strength concrete. All the slabs were 600 x 600 x 90 mm and
   contained different proportions of steel and plastic fibers. Out of a
   total number of 54 slabs, three slabs in each group were used as control
   specimens i.e. without fibers. The impact penetration tests were carried
   out using an air-gun system. The projectiles were made of hardened steel
   and were bi-conic in shape. Failures of the specimens were observed and
   size of the front and the rear face craters and the penetration depths
   were measured. The test results showed that the hybrid-fibers in the
   concrete lead to smaller crater volumes and reduce the spalling and
   scabbing damage. The hybrid-fibers arrest the crack development and thus
   minimize the size of the damaged area. The penetration depth and
   perforation thickness were predicted by modifying the impact function of
   NDRC equation to incorporate the effects of hybrid-fibers. The ballistic
   limit was also predicted. A simple formulation was then proposed for the
   prediction of the ejected concrete mass from the front and the rear
   faces of the specimens. Predictions matched well with the experimental
   observations. (C) 2013 Elsevier Ltd. All rights reserved.}},
Publisher = {{PERGAMON-ELSEVIER SCIENCE LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Abbas, H (Reprint Author), King Saud Univ, Dept Civil Engn, Riyadh 11421, Saudi Arabia.
   Almusallam, Tarek H.; Siddiqui, Nadeem A.; Iqbal, Rizwan A.; Abbas, Husain, King Saud Univ, Dept Civil Engn, Riyadh 11421, Saudi Arabia.}},
DOI = {{10.1016/j.ijimpeng.2013.02.005}},
ISSN = {{0734-743X}},
EISSN = {{1879-3509}},
Keywords = {{Hybrid-fibers; Steel fibers; Plastic fibers; Perforation; Non-deforming
   projectile}},
Keywords-Plus = {{HIGH-STRENGTH CONCRETE; MISSILE IMPACT; TARGETS; PENETRATION; PLATES;
   DAMAGE}},
Research-Areas = {{Engineering; Mechanics}},
Web-of-Science-Categories  = {{Engineering, Mechanical; Mechanics}},
Author-Email = {{abbas\_husain@hotmail.com}},
ResearcherID-Numbers = {{Almusallam, Tarek/E-7717-2014
   Abbas, Husain/J-5782-2012}},
ORCID-Numbers = {{Almusallam, Tarek/0000-0001-9614-9990
   Abbas, Husain/0000-0003-3865-9540}},
Funding-Acknowledgement = {{King Saud University {[}RGP-VPP-104]}},
Funding-Text = {{The Authors extend their appreciation to the Deanship of Scientific
   Research at King Saud University for funding the work through the
   research group project No. RGP-VPP-104. Thanks are also extended to the
   MMB Chair for Research and Studies in Strengthening and Rehabilitation
   of Structures, at the Depas talent of Civil Engineering, King Saud
   University for providing technical support.}},
Number-of-Cited-References = {{25}},
Times-Cited = {{25}},
Usage-Count-Last-180-days = {{7}},
Usage-Count-Since-2013 = {{46}},
Journal-ISO = {{Int. J. Impact Eng.}},
Doc-Delivery-Number = {{139LB}},
Unique-ID = {{ISI:000318583100002}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000319634600021,
Author = {Zhang, Zhifang and Shankar, Krishna and Ray, Tapabrata and Morozov,
   Evgeny V. and Tahtali, Murat},
Title = {{Vibration-based inverse algorithms for detection of delamination in
   composites}},
Journal = {{COMPOSITE STRUCTURES}},
Year = {{2013}},
Volume = {{102}},
Pages = {{226-236}},
Month = {{AUG}},
Abstract = {{Delamination is a frequent and potentially serious damage that can occur
   in laminated polymer composites due to the poor inter-laminar fracture
   toughness of the matrix. Vibration based detection methods employ
   changes caused by loss of stiffness in dynamic parameters such as
   frequencies to detect and assess damage. One of the challenges of using
   frequency shift for damage detection is that while the presence of
   damage is easily identified through a shift in measured frequency, the
   determination of the location and the severity of the damage are not
   easy to accomplish. To determine the location and severity of damage
   from measured changes in frequency, it is necessary to solve the inverse
   problem, which requires the solution of a set of non-linear simultaneous
   equations. In this paper, we examine three different inverse algorithms
   for solving the non-linear equations to predict the interface,
   lengthwise location and size of delamination: direct of solution using a
   graphical method, artificial neural network (ANN) and surrogate-based
   optimization. The three inverse algorithms have been validated using
   numerical data generated from the finite element model (FEM) of
   delaminated beams and measured frequencies from modal testing conducted
   on simply supported and cantilever carbon fiber reinforced beam
   specimens. Results show that all three algorithms can predict the
   delamination parameters accurately using the validation data directly
   generated from FE model. However, if using experimental data from real
   beams, ANN does not fare as well as the other two methods as it is more
   sensitive to the measurement errors. Finally, the advantages and
   limitations of each method have been summarized to provide a useful
   guide for selecting inverse algorithms for vibration-based delamination
   detection. (C) 2013 Elsevier Ltd. All rights reserved.}},
Publisher = {{ELSEVIER SCI LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, OXON, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Zhang, ZF (Reprint Author), Univ New S Wales, Sch Engn \& Informat Technol, Canberra, ACT 2600, Australia.
   Zhang, Zhifang; Shankar, Krishna; Ray, Tapabrata; Morozov, Evgeny V.; Tahtali, Murat, Univ New S Wales, Sch Engn \& Informat Technol, Canberra, ACT 2600, Australia.}},
DOI = {{10.1016/j.compstruct.2013.03.012}},
ISSN = {{0263-8223}},
Keywords = {{Delamination detection; Composite laminates; Vibration; Graphic
   technique; Surrogate-assisted optimization; Neural network}},
Keywords-Plus = {{STRUCTURAL DAMAGE DETECTION; ARTIFICIAL NEURAL-NETWORKS; GENETIC
   ALGORITHM; CRACK DETECTION; BEAMS; FREQUENCY; PREDICTION;
   IDENTIFICATION; MODEL}},
Research-Areas = {{Materials Science}},
Web-of-Science-Categories  = {{Materials Science, Composites}},
Author-Email = {{zhifang.zhang@student.adfa.edu.au
   k.shankar@-adfa.edu.au
   t.ray@adfa.edu.au
   e.morozov@adfa.edu.au
   m.tahtali@adfa.edu.au}},
ResearcherID-Numbers = {{Ray, Tapabrata/B-5664-2012
   }},
ORCID-Numbers = {{Ray, Tapabrata/0000-0003-1950-5917
   Morozov, Evgeny/0000-0003-3094-1269}},
Funding-Acknowledgement = {{UNSW Canberra; China Scholarship Council (CSC)}},
Funding-Text = {{Zhang thanks the UNSW Canberra and China Scholarship Council (CSC) for
   providing tuition waiver scholarship and living expenses for her PhD
   study in Australia.}},
Number-of-Cited-References = {{28}},
Times-Cited = {{25}},
Usage-Count-Last-180-days = {{0}},
Usage-Count-Since-2013 = {{17}},
Journal-ISO = {{Compos. Struct.}},
Doc-Delivery-Number = {{153WX}},
Unique-ID = {{ISI:000319634600021}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000318377900014,
Author = {Arteiro, A. and Catalanotti, G. and Xavier, J. and Camanho, P. P.},
Title = {{Notched response of non-crimp fabric thin-ply laminates}},
Journal = {{COMPOSITES SCIENCE AND TECHNOLOGY}},
Year = {{2013}},
Volume = {{79}},
Pages = {{97-114}},
Month = {{APR 18}},
Abstract = {{This paper presents an experimental investigation of the mechanical
   response of a new class of advanced composite materials manufactured
   using thin non-crimp fabrics. Tensile and compressive tests in both
   unnotched and notched specimens were performed using two different
   lay-ups. The notched tests were based on specimens with central cracks
   and with circular holes, loaded in tension and compression. Digital
   image correlation was used to monitor the onset and propagation of
   damage on the surface plies. The results show that the lay-up with
   blocked plies and with higher differences in fiber orientation angles
   between consecutive plies has lower unnotched strength. However, due to
   the larger fracture process zone observed in the notched tests, such
   lay-up has marginally higher notched strengths. A size effect on the
   strength was observed for both the open-hole tension and compression
   tests. The size effect and the associated notch sensitivity of thin
   non-crimp fabrics were similar to those observed in typical aerospace
   grade unidirectional pre-impregnated composite materials. It is also
   concluded that the thin non-crimp fabrics exhibit an improved response
   to bolt-bearing loads over traditional composite materials. (C) 2013
   Elsevier Ltd. All rights reserved.}},
Publisher = {{ELSEVIER SCI LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, OXON, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Camanho, PP (Reprint Author), Univ Porto, Fac Engn, DEMec, Rua Dr Roberto Frias, P-4200465 Oporto, Portugal.
   Arteiro, A.; Catalanotti, G.; Camanho, P. P., Univ Porto, Fac Engn, DEMec, P-4200465 Oporto, Portugal.
   Xavier, J., Univ Tras Os Montes \& Alto Douro, CITAB, P-5001801 Vila Real, Portugal.}},
DOI = {{10.1016/j.compscitech.2013.02.001}},
ISSN = {{0266-3538}},
Keywords = {{Laminates; Stress concentrations; Mechanical testing; Tow}},
Keywords-Plus = {{COMPOSITE-MATERIALS; MODEL; PREDICTION; STRENGTH; TENSILE}},
Research-Areas = {{Materials Science}},
Web-of-Science-Categories  = {{Materials Science, Composites}},
Author-Email = {{pcamanho@fe.up.pt}},
ResearcherID-Numbers = {{Xavier, Jose/A-4348-2013
   Catalanotti, Giuseppe/I-7833-2015
   }},
ORCID-Numbers = {{Xavier, Jose/0000-0002-7836-4598
   Catalanotti, Giuseppe/0000-0001-9326-9575
   Camanho, Pedro/0000-0003-0363-5207}},
Funding-Acknowledgement = {{Fundacao para a Ciencia e a Tecnologia {[}FCT-DFRH-SFRH-BPD-78104-2011]}},
Funding-Text = {{The authors acknowledge Chomarat (Ardeche, France), Aldila (Poway,
   California USA), VX Aerospace (Leesburg, Virginia USA), and Prof. S.W.
   Tsai (Stanford University, USA) for providing the material used in the
   experimental program carried out in this work. The authors also
   acknowledge Dr. Peter Linde and Dr. Stephane Mandi (Airbus) for the
   useful discussions. The second and third authors would like to
   acknowledge the suppor of the Fundacao para a Ciencia e a Tecnologia
   under the Grant FCT-DFRH-SFRH-BPD-78104-2011 and the Ciencia2008
   program, respectively.}},
Number-of-Cited-References = {{23}},
Times-Cited = {{25}},
Usage-Count-Last-180-days = {{0}},
Usage-Count-Since-2013 = {{20}},
Journal-ISO = {{Compos. Sci. Technol.}},
Doc-Delivery-Number = {{136QG}},
Unique-ID = {{ISI:000318377900014}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000315431500017,
Author = {Mughrabi, Hael},
Title = {{Cyclic slip irreversibility and fatigue life: A microstructure-based
   analysis}},
Journal = {{ACTA MATERIALIA}},
Year = {{2013}},
Volume = {{61}},
Number = {{4}},
Pages = {{1197-1203}},
Month = {{FEB}},
Abstract = {{The evolution of fatigue damage is intimately related to different types
   of more or less pronounced irreversible cyclic slip, associated with
   gradual permanent microstructural and topological changes which
   ultimately can cause fatigue failure. Only in a few cases has it been
   possible to assess quantitatively the cyclic slip irreversibility. Based
   on a limited amount of available experimental data amenable to analysis,
   an attempt is made in this work to explore whether there exists an
   explicit relationship between the cyclic slip irreversibility and
   fatigue life. The existence of such a relationship is suggested by a
   microstructure-based reformulation of the Coffin-Manson fatigue life
   law, which involves the cyclic slip irreversibility. The analysis of the
   experimental data in two adequately documented cases indicates that the
   cyclic slip irreversibility is related very satisfactorily to fatigue
   life via a power law which contains two constants. These two constants
   can be expressed in terms of the fatigue ductility coefficient and the
   fatigue ductility exponent of the Coffin-Manson fatigue life law. (C)
   2012 Acta Materialia Inc. Published by Elsevier Ltd. All rights
   reserved.}},
Publisher = {{PERGAMON-ELSEVIER SCIENCE LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Mughrabi, H (Reprint Author), Univ Erlangen Nurnberg, Dept Mat Sci \& Engn, Martensstr 5, D-91058 Erlangen, Germany.
   Univ Erlangen Nurnberg, Dept Mat Sci \& Engn, D-91058 Erlangen, Germany.}},
DOI = {{10.1016/j.actamat.2012.10.029}},
ISSN = {{1359-6454}},
Keywords = {{Cyclic deformation; Cyclic slip irreversibility; Fatigue damage; Fatigue
   life; Coffin-Manson fatigue life law}},
Keywords-Plus = {{ATOMIC-FORCE MICROSCOPY; SINGLE-CRYSTALS; CRACK INITIATION; ALPHA-IRON;
   DISLOCATION STRUCTURES; ALLOYS; METALS; DEFORMATION; NICKEL;
   POLYCRYSTALS}},
Research-Areas = {{Materials Science; Metallurgy \& Metallurgical Engineering}},
Web-of-Science-Categories  = {{Materials Science, Multidisciplinary; Metallurgy \& Metallurgical
   Engineering}},
Author-Email = {{mughrabi@ww.uni-erlangen.de}},
Number-of-Cited-References = {{28}},
Times-Cited = {{25}},
Usage-Count-Last-180-days = {{3}},
Usage-Count-Since-2013 = {{54}},
Journal-ISO = {{Acta Mater.}},
Doc-Delivery-Number = {{096UZ}},
Unique-ID = {{ISI:000315431500017}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000310572200023,
Author = {Wang, H. T. and Wang, G. Z. and Xuan, F. Z. and Tu, S. T.},
Title = {{An experimental investigation of local fracture resistance and crack
   growth paths in a dissimilar metal welded joint}},
Journal = {{MATERIALS \& DESIGN}},
Year = {{2013}},
Volume = {{44}},
Pages = {{179-189}},
Month = {{FEB}},
Abstract = {{An experimental investigation on the local fracture resistance and crack
   growth behavior in a Alloy52M dissimilar metal welded joint (DMWJ)
   between A508 ferritic steel and 316L stainless steel has been carried
   out by using the single-edge notched bend (SENB) specimens. The local
   J-resistance curves and crack growth paths of 13 cracks located at
   various positions in the DMWJ were determined, and the effects of the
   local strength mismatch on local fracture resistance, crack growth paths
   and integrity assessment for the DMWJ were analyzed. The results show
   that the cracks always deviate to the materials with lower strength, and
   the crack path deviations are mainly controlled by the strength
   mismatch, rather than toughness mismatch. The J-resistance curve with
   larger crack path deviation only reflect the apparent fracture
   resistance along the crack growth region, rather than the intrinsic
   fracture resistance of the material at the initial crack-tip region.
   Without considering the local fracture resistance properties of heat
   affected zone (HAZ), interface and near interface zone, the use of the
   J-resistance curves of base metals or weld metals following present
   codes will unavoidably produce non-conservative (unsafe) or excessive
   conservative assessment results. In most cases, the assessment results
   will be potentially unsafe. Therefore, it is recommended to obtain and
   use local mechanical and fracture resistance properties of all regions
   of the DMWJ if the complex local mismatch situation is a concern. And
   new integrity assessment methods based on local damage and fracture
   models also need to be developed for the DMWJs. (C) 2012 Elsevier Ltd.
   All rights reserved.}},
Publisher = {{ELSEVIER SCI LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, OXON, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Wang, GZ (Reprint Author), E China Univ Sci \& Technol, MOE Key Lab Pressurized Syst \& Safety, Sch Mech \& Power Engn, Shanghai 200237, Peoples R China.
   Wang, H. T.; Wang, G. Z.; Xuan, F. Z.; Tu, S. T., E China Univ Sci \& Technol, MOE Key Lab Pressurized Syst \& Safety, Sch Mech \& Power Engn, Shanghai 200237, Peoples R China.}},
DOI = {{10.1016/j.matdes.2012.07.067}},
ISSN = {{0261-3069}},
Keywords = {{Local fracture resistance; Crack growth path; Strength mismatch;
   Dissimilar metal welded joint; Integrity assessment}},
Keywords-Plus = {{MECHANICAL HETEROGENEITY; LIMIT LOADS; ALLOY; SPECIMENS; WELDMENTS;
   BEHAVIOR; FAILURE; STEEL; CURVE}},
Research-Areas = {{Materials Science}},
Web-of-Science-Categories  = {{Materials Science, Multidisciplinary}},
Author-Email = {{gzwang@ecust.edu.cn}},
ResearcherID-Numbers = {{xuan, fu-zhen/L-5683-2016}},
Funding-Acknowledgement = {{National Natural Science Foundation of China {[}51075149, 50835003];
   National High Technology Research and Development Program of China
   {[}2009AA044803]}},
Funding-Text = {{This work was financially supported by the Projects of the National
   Natural Science Foundation of China (51075149 and 50835003), and
   National High Technology Research and Development Program of China
   (2009AA044803).}},
Number-of-Cited-References = {{30}},
Times-Cited = {{25}},
Usage-Count-Last-180-days = {{6}},
Usage-Count-Since-2013 = {{34}},
Journal-ISO = {{Mater. Des.}},
Doc-Delivery-Number = {{030LM}},
Unique-ID = {{ISI:000310572200023}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000327906200036,
Author = {Michel, A. and Solgaard, A. O. S. and Pease, B. J. and Geiker, M. R. and
   Stang, H. and Olesen, J. F.},
Title = {{Experimental investigation of the relation between damage at the
   concrete-steel interface and initiation of reinforcement corrosion in
   plain and fibre reinforced concrete}},
Journal = {{CORROSION SCIENCE}},
Year = {{2013}},
Volume = {{77}},
Pages = {{308-321}},
Month = {{DEC}},
Abstract = {{Cracks in covering concrete are known to hasten initiation of steel
   corrosion in reinforced concrete structures. To minimise the impact of
   cracks on the deterioration of reinforced concrete structures, current
   approaches in (inter)national design codes often limit the concrete
   surface crack width. Recent investigations however, indicate that the
   concrete-reinforcement interfacial condition is a more fundamental
   criterion related to reinforcement corrosion. This work investigates the
   relation between macroscopic damage at the concrete-steel interface and
   corrosion initiation of reinforcement embedded in plain and fibre
   reinforced concrete. Comparisons of experimental and numerical results
   indicate a strong correlation between corrosion initiation and
   interfacial condition. (C) 2013 Elsevier Ltd. All rights reserved.}},
Publisher = {{PERGAMON-ELSEVIER SCIENCE LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Michel, A (Reprint Author), Tech Univ Denmark DTU, Dept Civil Engn, Lyngby, Denmark.
   Michel, A.; Solgaard, A. O. S.; Pease, B. J.; Geiker, M. R.; Stang, H.; Olesen, J. F., Tech Univ Denmark DTU, Dept Civil Engn, Lyngby, Denmark.
   Solgaard, A. O. S., COWI AS Denmark, Lyngby, Denmark.
   Michel, A.; Geiker, M. R., Norwegian Univ Sci \& Technol NTNU, Dept Struct Engn, Trondheim, Norway.}},
DOI = {{10.1016/j.corsci.2013.08.019}},
ISSN = {{0010-938X}},
EISSN = {{1879-0496}},
Keywords = {{Steel reinforced concrete; Atmospheric corrosion}},
Keywords-Plus = {{CHLORIDE-INDUCED CORROSION; HIGH-PERFORMANCE CONCRETE; CRACK WIDTH;
   SPLITTING TEST; MODEL; PERMEABILITY; AREAS; RATES; WATER}},
Research-Areas = {{Materials Science; Metallurgy \& Metallurgical Engineering}},
Web-of-Science-Categories  = {{Materials Science, Multidisciplinary; Metallurgy \& Metallurgical
   Engineering}},
Author-Email = {{almic@byg.dtu.dk}},
ResearcherID-Numbers = {{Pease, Brad/A-4703-2012
   }},
ORCID-Numbers = {{Pease, Brad/0000-0001-7088-3126
   Olesen, John Forbes/0000-0001-6695-7719
   Michel, Alexander/0000-0002-5934-8488
   Stang, Henrik/0000-0002-5812-4028
   Geiker, Mette Rica/0000-0003-4952-8394}},
Funding-Acknowledgement = {{Femern Baelt A/S; Sund \& Baelt Holding A/S; Danish Agency for Science,
   Technology and Innovation; COWI A/S; DTU; Bekaert NV; Grace; Danish Road
   Directorate; Danish Expert Centre for Infrastructure; COIN (COncrete
   INnovation centre)}},
Funding-Text = {{The first author gratefully acknowledges the financial support of Femern
   Baelt A/S, Sund \& Baelt Holding A/S and The Danish Agency for Science,
   Technology and Innovation as well as COIN (COncrete INnovation centre,
   www.coinweb.no) and its partners for facilitating the research behind
   this paper. Financial supports of the Ph.D. study ``Application of Fibre
   Reinforced Concrete in Civil Infrastructure{''} by the Danish Agency for
   Science, Technology and Innovation, COWI A/S, DTU, Bekaert NV, Grace,
   and the Danish Road Directorate are also acknowledged as well as
   financial contributions from the Danish Expert Centre for
   Infrastructure.}},
Number-of-Cited-References = {{67}},
Times-Cited = {{24}},
Usage-Count-Last-180-days = {{1}},
Usage-Count-Since-2013 = {{16}},
Journal-ISO = {{Corrosion Sci.}},
Doc-Delivery-Number = {{264UJ}},
Unique-ID = {{ISI:000327906200036}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000323402600037,
Author = {Zhang, Zhongpu and Guazzato, Massimiliano and Sornusuwan, Tanapon and
   Scherrer, Susanne S. and Rungsiyakull, Chaiy and Li, Wei and Swain,
   Michael V. and Li, Qing},
Title = {{Thermally induced fracture for core-veneered dental ceramic structures}},
Journal = {{ACTA BIOMATERIALIA}},
Year = {{2013}},
Volume = {{9}},
Number = {{9}},
Pages = {{8394-8402}},
Month = {{SEP}},
Abstract = {{Effective and reliable clinical uses of dental ceramics necessitate an
   insightful analysis of the fracture behaviour under critical conditions.
   To better understand failure characteristics of porcelain veneered to
   zirconia core ceramic structures, thermally induced cracking during the
   cooling phase of fabrication is studied here by using the extended
   finite element method (XFEM). In this study, a transient thermal
   analysis of cooling is conducted first to determine the temperature
   distributions. The time-dependent temperature field is then imported to
   the XFEM model for viscoelastic thermomechanical analysis, which
   predicts thermally induced damage and cracking at different time steps.
   Temperature-dependent material properties are used in both transient
   thermal and thermomechanical analyses. Three typical ceramic structures
   are considered in this paper, namely bi-layered spheres, squat cylinders
   and dental crowns with thickness ratios of either 1:2 or 1:1. The XFEM
   fracture patterns exhibit good agreement with clinical observation and
   the in vitro experimental results obtained from scanning electron
   microscopy characterization. The study reveals that fast cooling can
   lead to thermal fracture of these different bi-layered ceramic
   structures, and cooling rate (in terms of heat transfer coefficient)
   plays a critical role in crack initiation and propagation. By exploring
   different cooling rates, the heat transfer coefficient thresholds of
   fracture are determined for different structures, which are of clear
   clinical implication. (C) 2013 Acta Materialia Inc. Published by
   Elsevier Ltd. All rights reserved.}},
Publisher = {{ELSEVIER SCI LTD}},
Address = {{THE BOULEVARD, LANGFORD LANE, KIDLINGTON, OXFORD OX5 1GB, OXON, ENGLAND}},
Type = {{Article}},
Language = {{English}},
Affiliation = {{Li, Q (Reprint Author), Univ Sydney, Fac Engn, Sch Aerosp Mech \& Mechatron Engn, Sydney, NSW 2006, Australia.
   Zhang, Zhongpu; Rungsiyakull, Chaiy; Li, Wei; Li, Qing, Univ Sydney, Fac Engn, Sch Aerosp Mech \& Mechatron Engn, Sydney, NSW 2006, Australia.
   Guazzato, Massimiliano, Univ Sydney, Westmead Hosp, Westmead Ctr Oral Hlth, Discipline Prosthodont,Fac Dent, Sydney, NSW 2006, Australia.
   Sornusuwan, Tanapon; Swain, Michael V., Univ Sydney, Fac Dent, Discipline Biomat, Sydney, NSW 2006, Australia.
   Scherrer, Susanne S., Univ Geneva, Dept Prosthodont Biomat, Geneva, Switzerland.}},
DOI = {{10.1016/j.actbio.2013.05.009}},
ISSN = {{1742-7061}},
Keywords = {{XFEM; Thermomechanical; Thermal fracture; Bi-layered ceramic; Dental
   prosthesis}},
Keywords-Plus = {{FINITE-ELEMENT-METHOD; NONCARIOUS CERVICAL LESIONS; FIXED PARTIAL
   DENTURES; X-FEM; CRACK-GROWTH; NUMERICAL-SIMULATION; RESIDUAL-STRESSES;
   FAILURE ANALYSIS; LEVEL SETS; PART II}},
Research-Areas = {{Engineering; Materials Science}},
Web-of-Science-Categories  = {{Engineering, Biomedical; Materials Science, Biomaterials}},
Author-Email = {{qing.li@sydney.edu.au}},
ResearcherID-Numbers = {{Swain, Michael/J-7266-2017}},
Funding-Acknowledgement = {{Australian Research Council (ARC)}},
Funding-Text = {{The support from Australian Research Council (ARC) is acknowledged. The
   authors acknowledge the facilities, and the scientific and technical
   assistance of the Australian Microscopy \& Microanalysis Research
   Facility in The University of Sydney. We appreciate all the anonymous
   reviewers for their constructive comments and suggestions in the early
   versions of this paper.}},
Number-of-Cited-References = {{65}},
Times-Cited = {{24}},
Usage-Count-Last-180-days = {{2}},
Usage-Count-Since-2013 = {{34}},
Journal-ISO = {{Acta Biomater.}},
Doc-Delivery-Number = {{204WS}},
Unique-ID = {{ISI:000323402600037}},
OA = {{No}},
DA = {{2017-08-29}},
}

@article{ ISI:000322706000009,
Author = {Riccio, A. and Raimondo, A. and Scaramuzzino, F.},
Title = {{A Study on Skin Delaminations Growth in Stiffened Composite Panels by a
   Novel Numerical Approach}},
Journal = {{APPLIED COMPOSITE MATERIALS}},
Year = {{2013}},
Volume = {{20}},
Number = {{4}},
Pages = {{465-488}},
Month = {{AUG}},
Abstract = {{In this paper, a study on skin delamination growth in stiffened
   composite panels made of carbon fibres reinforced polymers and subjected
   to compressive load is presented. A robust (mesh and time step
   independent) numerical finite elements procedure, based on the Virtual
   Crack Closure Technique (VCCT) and on the fail release approach, is used
   here to investigate the influence of skin delamination size and position
   on the damage tolerance of stiffened composite panels. Four stiffened
   panels configurations with skin delaminations differently sized and
   positioned are introduced. Bay delaminations and delaminations under the
   stringer foot are considered. The novel numerical procedure has been
   used to

repository: OpenDataExpMechanics/Survey

repo_name: OpenDataExpMechanics/Survey