Interaction of delaminations and matrix cracks in a CFRP plate, Part II: Simulation using an enriched shell finite element model

Numerical simulations are presented of a recently developed test which creates multiple delaminations in a CFRP laminate specimen that grow and interact via transverse matrix cracks [1]. A novel shell element enriched with the Floating Node Method, and a damage algorithm based on the Virtual Crack C...

Full description

Saved in:
Bibliographic Details
Published inComposites. Part A, Applied science and manufacturing Vol. 103; pp. 252 - 262
Main Authors McElroy, Mark W., Gutkin, Renaud, Pankow, Mark
Format Journal Article
LanguageEnglish
Published Langley Research Center Elsevier Ltd 01.12.2017
Elsevier
Subjects
Online AccessGet full text

Cover

Loading…
Abstract Numerical simulations are presented of a recently developed test which creates multiple delaminations in a CFRP laminate specimen that grow and interact via transverse matrix cracks [1]. A novel shell element enriched with the Floating Node Method, and a damage algorithm based on the Virtual Crack Closure Technique, were used to successfully simulate the tests. Additionally, a 3D high mesh fidelity model based on cohesive zones and continuum damage mechanics was used to simulate the tests and act as a representative of other similar state-of-the-art high mesh fidelity modeling techniques to compare to the enriched shell element. The enriched shell and high mesh fidelity models had similar levels of accuracy and generally matched the experimental data. With runtimes of 36 min for the shell model and 55 h for the high mesh fidelity model, the shell model is 92 times faster than the high-fidelity simulation.
AbstractList Numerical simulations are presented of a recently developed test which creates multiple delaminations in a CFRP laminate specimen that grow and interact via transverse matrix cracks [1]. A novel shell element enriched with the Floating Node Method, and a damage algorithm based on the Virtual Crack Closure Technique, were used to successfully simulate the tests. Additionally, a 3D high mesh fidelity model based on cohesive zones and continuum damage mechanics was used to simulate the tests and act as a representative of other similar state-of-the-art high mesh fidelity modeling techniques to compare to the enriched shell element. The enriched shell and high mesh fidelity models had similar levels of accuracy and generally matched the experimental data. With runtimes of 36 min for the shell model and 55 h for the high mesh fidelity model, the shell model is 92 times faster than the high-fidelity simulation.
Numerical simulations are presented of a recently developed test which creates multiple delaminations in a CFRP laminate specimen that grow and interact via transverse matrix cracks [1]. A novel shell element enriched with the Floating Node Method, and a damage algorithm based on the Virtual Crack Closure Technique, were used to successfully simulate the tests. Additionally, a 3D high mesh fidelity model based on cohesive zones and continuum damage mechanics was used to simulate the tests and act as a representative of other similar state-of-the-art high mesh fidelity modeling techniques to compare to the enriched shell element. The enriched shell and high mesh fidelity models had similar levels of accuracy and generally matched the experimental data. With runtimes of 36 minutes for the shell model and 55 hours for the high mesh fidelity model, the shell model is 92 times faster than the high-fidelity simulation.
Numerical simulations are presented of a recently developed test which creates multiple delaminations in a CFRP laminate specimen that grow and interact via transverse matrix cracks [ 1 ]. A novel shell element enriched with the Floating Node Method, and a damage algorithm based on the Virtual Crack Closure Technique, were used to successfully simulate the tests. Additionally, a 3D high mesh fidelity model based on cohesive zones and continuum damage mechanics was used to simulate the tests and act as a representative of other similar state-of-the-art high mesh fidelity modeling techniques to compare to the enriched shell element. The enriched shell and high mesh fidelity models had similar levels of accuracy and generally matched the experimental data. With runtimes of 36 minutes for the shell model and 55 hours for the high mesh fidelity model, the shell model is 92 times faster than the high-fidelity simulation.
Numerical simulations are presented of a recently developed test which creates multiple delaminations in a CFRP laminate specimen that grow and interact via transverse matrix cracks. A novel shell element enriched with the Floating Node Method, and a damage algorithm based on the Virtual Crack Closure Technique, were used to successfully simulate the tests. Additionally, a 3D high mesh fidelity model based on cohesive zones and continuum damage mechanics was used to simulate the tests and act as a representative of other similar state-of-the-art high mesh fidelity modeling techniques to compare to the enriched shell element. The enriched shell and high mesh fidelity models had similar levels of accuracy and generally matched the experimental data. With runtimes of 36 minutes for the shell model and 55 hours for the high mesh fidelity model, the shell model is 92 times faster than the high- fidelity simulation.
Audience PUBLIC
Author McElroy, Mark W.
Pankow, Mark
Gutkin, Renaud
AuthorAffiliation 3 North Carolina State University, Raleigh, NC
2 Volvo Cars, Gothenburg, Sweden
1 NASA Langley Research Center, 2 W. Reid St, Mail Stop 188E, Hampton, VA 23451
AuthorAffiliation_xml – name: 2 Volvo Cars, Gothenburg, Sweden
– name: 1 NASA Langley Research Center, 2 W. Reid St, Mail Stop 188E, Hampton, VA 23451
– name: 3 North Carolina State University, Raleigh, NC
Author_xml – sequence: 1
  givenname: Mark W.
  surname: McElroy
  fullname: McElroy, Mark W.
  email: mark.w.mcelroy@nasa.gov
  organization: NASA Langley Research Center, 2 W. Reid St, Mail Stop 188E, Hampton, VA 23681, United States
– sequence: 2
  givenname: Renaud
  surname: Gutkin
  fullname: Gutkin, Renaud
  organization: Volvo Car Corporation, Durability CAE Body & Trim, Sweden
– sequence: 3
  givenname: Mark
  surname: Pankow
  fullname: Pankow, Mark
  organization: North Carolina State University, Raleigh, NC 27695, United States
BackLink https://www.ncbi.nlm.nih.gov/pubmed/33479561$$D View this record in MEDLINE/PubMed
BookMark eNqNUU1v1DAUtFAR_eIfIGRuHMhix3HscEBCKworVaKircTN8tovXS-JvbWdCm78dBy2VOXGyR8z8968N8fowAcPCL2iZEEJbd9uFyaMu5BchqQXNaGi_C8IaZ-gIyqFrLhsyEG5M95VkvFvh-g4pS0hhLGOPkOHjDWi4y09Qr9WPkPUJrvgceixhUGPzuv5nbD2Fo86R_cDm0L6nrDzWOPl2dcLvBt0hjf4QseMV6t3-NKN0_BHh6fk_E0RY_DRmQ1YnDYwDLh3vljGMMAIPuMxlG6n6GmvhwTP788TdH328Wr5uTr_8mm1_HBeGS5IrrjoGa2JhZY3II3llPLe0Gbdm1Zq3ddCamY6Ljitu3VnjKZA1ratGQUuuWUn6P2-7m5aj2BNMRD1oHbRjTr-VEE79S_i3UbdhDslJG1lTUqB1_cFYridIGU1umTKWNpDmJKqG1nWy0UrCrXbU00MKUXoH9pQouYE1VY9SlDNCc5QSbBoXz72-aD8G1khvNgTvC7S4jXN-o6QugzfFHi5h6Es885BVMk48Aasi2CyssH9h4vfP5m__g
CitedBy_id crossref_primary_10_1016_j_compositesa_2021_106790
crossref_primary_10_1115_1_4050619
crossref_primary_10_1177_00219983221082039
crossref_primary_10_1016_j_compositesa_2017_09_011
crossref_primary_10_1016_j_compositesa_2018_10_004
crossref_primary_10_1016_j_compositesa_2021_106377
crossref_primary_10_1016_j_compositesa_2021_106795
crossref_primary_10_1016_j_compstruct_2021_113945
crossref_primary_10_1016_j_compstruct_2022_116549
crossref_primary_10_1016_j_cma_2019_03_041
crossref_primary_10_1016_j_cma_2018_12_004
crossref_primary_10_1016_j_compstruct_2021_114196
crossref_primary_10_1016_j_engfracmech_2018_12_009
Cites_doi 10.1016/S0266-3538(97)00146-2
10.1016/j.compositesa.2015.01.021
10.1016/j.compstruct.2012.05.015
10.1016/j.compositesa.2010.02.011
10.1016/j.cma.2003.08.009
10.1016/j.compositesa.2017.09.011
10.1016/j.compstruct.2017.01.057
10.1016/0266-3538(96)00005-X
10.1016/j.engfracmech.2014.05.018
10.1177/0021998313499475
10.1007/s11837-011-0053-y
10.1016/j.compscitech.2007.02.005
10.1016/0013-7944(77)90013-3
10.1016/j.compscitech.2014.10.001
10.1177/0021998312454478
10.1016/j.compstruct.2012.03.039
10.1016/j.compositesa.2015.08.026
10.1016/0020-7683(89)90021-8
10.1016/0961-9526(94)00097-S
10.1007/s11837-008-0081-4
10.1016/j.compstruct.2013.09.004
10.1016/j.wear.2004.01.008
10.1007/s11837-006-0223-5
10.1177/002199837701100409
10.1115/1.4004694
10.1177/0021998311410473
10.1016/j.compstruct.2015.10.028
10.1016/0266-3538(94)00079-4
10.1016/j.compositesa.2013.07.004
10.1016/j.compstruct.2015.12.036
10.1002/nme.3195
10.1016/j.compstruct.2015.02.055
10.2514/1.32832
10.1016/j.compscitech.2012.08.019
10.1016/j.ijimpeng.2009.04.006
10.1007/s11029-007-0002-6
10.1016/S1359-835X(00)00133-0
10.1007/s10704-010-9506-5
10.1016/S1359-8368(98)00013-4
10.2514/1.J051773
10.1016/S0263-8223(96)00079-7
ContentType Journal Article
Copyright 2017
Copyright Determination: PUBLIC_USE_PERMITTED
Copyright_xml – notice: 2017
– notice: Copyright Determination: PUBLIC_USE_PERMITTED
DBID CYE
CYI
NPM
AAYXX
CITATION
7X8
5PM
DOI 10.1016/j.compositesa.2017.10.006
DatabaseName NASA Scientific and Technical Information
NASA Technical Reports Server
PubMed
CrossRef
MEDLINE - Academic
PubMed Central (Full Participant titles)
DatabaseTitle PubMed
CrossRef
MEDLINE - Academic
DatabaseTitleList
PubMed


MEDLINE - Academic
Database_xml – sequence: 1
  dbid: NPM
  name: PubMed
  url: https://proxy.k.utb.cz/login?url=http://www.ncbi.nlm.nih.gov/entrez/query.fcgi?db=PubMed
  sourceTypes: Index Database
DeliveryMethod fulltext_linktorsrc
Discipline Engineering
EISSN 1878-5840
EndPage 262
ExternalDocumentID 10_1016_j_compositesa_2017_10_006
33479561
20190025754
S1359835X17303640
Genre Journal Article
GrantInformation 826611.04.07.01
ARMD_826611
GrantInformation_xml – fundername: Aeronautics NASA
GroupedDBID --K
--M
.~1
0R~
1B1
1~.
1~5
29F
4.4
457
4G.
5GY
5VS
6TJ
7-5
71M
8P~
AABNK
AABXZ
AACTN
AAEDT
AAEDW
AAEPC
AAIAV
AAIKJ
AAKOC
AALRI
AAOAW
AAQFI
AAQXK
AAXUO
ABFNM
ABMAC
ABXDB
ABXRA
ABYKQ
ACDAQ
ACGFS
ACNNM
ACRLP
ADBBV
ADEZE
ADIYS
ADMUD
AEBSH
AEKER
AEZYN
AFKWA
AFRZQ
AFTJW
AGHFR
AGUBO
AGYEJ
AIEXJ
AIKHN
AITUG
AJBFU
AJOXV
ALMA_UNASSIGNED_HOLDINGS
AMFUW
AMRAJ
ASPBG
AVWKF
AXJTR
AZFZN
BKOJK
BLXMC
CS3
EBS
EFJIC
EFLBG
EJD
EO8
EO9
EP2
EP3
F5P
FDB
FEDTE
FGOYB
FIRID
FNPLU
FYGXN
G-Q
GBLVA
HVGLF
HZ~
IHE
J1W
KOM
M41
MAGPM
MO0
N9A
O-L
O9-
OAUVE
OZT
P-8
P-9
P2P
PC.
Q38
R2-
RIG
RNS
ROL
RPZ
SDF
SDG
SDP
SES
SEW
SPC
SPCBC
SSM
SSZ
T5K
TN5
ZMT
~G-
AAHBH
AAXKI
CYE
CYI
AFJKZ
NPM
AAYXX
CITATION
7X8
5PM
ID FETCH-LOGICAL-c570t-57f3120de654e8cd5115fc14bfc68aaf278a3c9575129b9cca1e0bd6231e585d3
IEDL.DBID .~1
ISSN 1359-835X
IngestDate Tue Sep 17 21:21:33 EDT 2024
Sat Oct 26 05:53:17 EDT 2024
Thu Sep 26 18:26:51 EDT 2024
Thu Oct 24 09:37:25 EDT 2024
Fri Oct 18 14:47:31 EDT 2024
Fri Feb 23 02:27:34 EST 2024
IsDoiOpenAccess true
IsOpenAccess true
IsPeerReviewed true
IsScholarly true
Keywords D. Finite element analysis (FEA)
C. Fracture
B. Delamination
A. Laminates
B. Fracture
C. Finite element analysis (FEA)
Language English
LinkModel DirectLink
MergedId FETCHMERGED-LOGICAL-c570t-57f3120de654e8cd5115fc14bfc68aaf278a3c9575129b9cca1e0bd6231e585d3
Notes Langley Research Center
NF1676L-26156
LaRC
ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 23
OpenAccessLink https://ntrs.nasa.gov/citations/20190025754
PMID 33479561
PQID 2480335767
PQPubID 23479
PageCount 11
ParticipantIDs pubmedcentral_primary_oai_pubmedcentral_nih_gov_7816820
proquest_miscellaneous_2480335767
crossref_primary_10_1016_j_compositesa_2017_10_006
pubmed_primary_33479561
nasa_ntrs_20190025754
elsevier_sciencedirect_doi_10_1016_j_compositesa_2017_10_006
PublicationCentury 2000
PublicationDate 2017-12-01
PublicationDateYYYYMMDD 2017-12-01
PublicationDate_xml – month: 12
  year: 2017
  text: 2017-12-01
  day: 01
PublicationDecade 2010
PublicationPlace Langley Research Center
PublicationPlace_xml – name: Langley Research Center
– name: England
PublicationTitle Composites. Part A, Applied science and manufacturing
PublicationTitleAlternate Compos Part A Appl Sci Manuf
PublicationYear 2017
Publisher Elsevier Ltd
Elsevier
Publisher_xml – name: Elsevier Ltd
– name: Elsevier
References Apelian (b0035) 2008; 60
De Carvalho, Chen, Pinho, Ratcliffe, Baiz, Tay (b0200) 2015; 71
Ratcliffe J, Czabaj M, O’Brien T. A test for characterizing delamination migration in carbon/epoxy tape laminates NASA/TM-2013-218028. NASA; 2013.
Brouzoulis, Fagerström (b0155) 2015; 126
Hinton, Kaddour, Soden (b0010) 2004
Rybicki, Schmueser, Fox (b0040) 1977; 11
O’Brien T, Johnston W, Toland G. Mode II interlaminar fracture toughness and fatigue characterization of a graphite epoxy composite material, NASA/TM 2010-216838. NASA; 2010.
Olsson, Thesken, Brandt, Jonsson, Nilsson (b0240) 1997; 36
Heimbs S, Heller S, Middendorf P. Simulation of low velocity impact on composite plates with compressive preload. In: 7th German LS-DYNA forum. Bamberg, Germany, September, 2008.
Bouvet, Rivallant, Barrau (b0110) 2012; 72
Allison (b0025) 2011; 63
Davies G, Robinson P. Predicting failure by debonding/delamination. In: AGARD: 74th structures and materials meeting, debonding/delamination of composites, Patras, Greece, May 24–29; 1992.
Wisnom (b0070) 2010; 41
Chen, Pinho, De Carvalho, Baiz, Tay (b0175) 2014; 127
Orifici, Thomson, Degenhardt, Bisagni, Bayandor (b0185) 2007; 43
Zhou, Fang, Cox, Yang (b0100) 2010; 165
Camanho, Maimí, Dávila (b0230) 2007; 67
Främby, Brouzoulis, Fagerström (b0255) 2016; 140
Qiao, Chen, Yang, Lua (b0130) 2011; 133
Swindeman, Iarve, Brockman, Mollenhauer, Hallett (b0095) 2013; 51
Benzeggagh, Kenane (b0195) 1996; 56
Kaddour, Hinton, Smith, Li (b0015) 2013; 47
McElroy M. An enriched shell finite element for progressive damage simulation in composite laminates, NASA/TM 2016-219211. NASA; 2016.
McElroy (b0170) 2017; 167
Heimbs, Heller, Middendorf, Hähnel, Weiße (b0125) 2009; 36
Brouzoulis J, Fagerström M. Modelling of multiple delaminations in shells using XFEM. In: Proceedings for the 19th international conference on composite materials (ICCM19); 2013.
O’Brien (b0045) 1982; 775
Collombet, Lalbin, Lataillade (b0055) 1998; 58
Rybicki, Kanninen (b0065) 1977; 9
Allison, Backman, Christodoulou (b0030) 2006; 58
Dassault Systems. Abaqus 6.13 Analysis User Manual; 2013.
Canturri, Greenhalgh, Pinho, Ankersen (b0225) 2013; 54
Geubelle, Baylor (b0060) 1998; 29
Krueger, O’Brien (b0115) 2001; 32
Iarve, Gurvich, Mollenhauer, Rose, Dávila (b0090) 2011; 88
Canturri, Greenhalgh, Pinho (b0215) 2014; 105
Schön (b0245) 2004; 257
Zheng, Sun (b0140) 1995; 53
Molker H, Gutkin R, Pinho S, Asp L. Identifying failure initiation in automotive structures made of NCF reinforced composites for hot spot analysis. In: Proceedings of the 17th European conference on composites materials. Munich, Germany, June 26–30, 2016.
McElroy, Leone, Ratcliffe, Czabaj, Yuan (b0210) 2015; 79
McElroy, Jackson, Olsson, Hellstrom, Tsampas, Pankow (b0005) 2017; 103
Shi, Swait, Soutis (b0080) 2012; 94
Wang, Raju, Sleight (b0190) 1995; 5
González, Maimí, Camanho, Turon, Mayugo (b0075) 2012; 94
Van der Meer, Sluys, Hallett, Wisnom (b0105) 2012; 46
Larsson (b0145) 2004; 193
Feng, Aymerich (b0085) 2014; 108
Dávila, Camanho, Turon (b0135) 2008; 45
Rose C, Dávila C, Leone F. Analysis methods for progressive damage of composite structures. NASA/TM 2013-218024. NASA; 2013.
Ming-Yuan, Hutchinson (b0260) 1989; 25
Brouzoulis, Fagerström, Svenning (b0160) 2016; 136
Pinho, Darvizeh, Robinson, Schuecker, Camanho (b0220) 2012; 46
Shi (10.1016/j.compositesa.2017.10.006_b0080) 2012; 94
10.1016/j.compositesa.2017.10.006_b0150
Zhou (10.1016/j.compositesa.2017.10.006_b0100) 2010; 165
Larsson (10.1016/j.compositesa.2017.10.006_b0145) 2004; 193
De Carvalho (10.1016/j.compositesa.2017.10.006_b0200) 2015; 71
Hinton (10.1016/j.compositesa.2017.10.006_b0010) 2004
10.1016/j.compositesa.2017.10.006_b0235
Främby (10.1016/j.compositesa.2017.10.006_b0255) 2016; 140
Iarve (10.1016/j.compositesa.2017.10.006_b0090) 2011; 88
Apelian (10.1016/j.compositesa.2017.10.006_b0035) 2008; 60
Rybicki (10.1016/j.compositesa.2017.10.006_b0040) 1977; 11
Dávila (10.1016/j.compositesa.2017.10.006_b0135) 2008; 45
McElroy (10.1016/j.compositesa.2017.10.006_b0005) 2017; 103
McElroy (10.1016/j.compositesa.2017.10.006_b0210) 2015; 79
González (10.1016/j.compositesa.2017.10.006_b0075) 2012; 94
Brouzoulis (10.1016/j.compositesa.2017.10.006_b0155) 2015; 126
Heimbs (10.1016/j.compositesa.2017.10.006_b0125) 2009; 36
McElroy (10.1016/j.compositesa.2017.10.006_b0170) 2017; 167
10.1016/j.compositesa.2017.10.006_b0180
Brouzoulis (10.1016/j.compositesa.2017.10.006_b0160) 2016; 136
Olsson (10.1016/j.compositesa.2017.10.006_b0240) 1997; 36
10.1016/j.compositesa.2017.10.006_b0020
Camanho (10.1016/j.compositesa.2017.10.006_b0230) 2007; 67
Wang (10.1016/j.compositesa.2017.10.006_b0190) 1995; 5
Allison (10.1016/j.compositesa.2017.10.006_b0025) 2011; 63
10.1016/j.compositesa.2017.10.006_b0050
Krueger (10.1016/j.compositesa.2017.10.006_b0115) 2001; 32
Feng (10.1016/j.compositesa.2017.10.006_b0085) 2014; 108
Wisnom (10.1016/j.compositesa.2017.10.006_b0070) 2010; 41
10.1016/j.compositesa.2017.10.006_b0250
Chen (10.1016/j.compositesa.2017.10.006_b0175) 2014; 127
Swindeman (10.1016/j.compositesa.2017.10.006_b0095) 2013; 51
10.1016/j.compositesa.2017.10.006_b0205
Canturri (10.1016/j.compositesa.2017.10.006_b0215) 2014; 105
Qiao (10.1016/j.compositesa.2017.10.006_b0130) 2011; 133
Schön (10.1016/j.compositesa.2017.10.006_b0245) 2004; 257
Pinho (10.1016/j.compositesa.2017.10.006_b0220) 2012; 46
Canturri (10.1016/j.compositesa.2017.10.006_b0225) 2013; 54
Kaddour (10.1016/j.compositesa.2017.10.006_b0015) 2013; 47
Orifici (10.1016/j.compositesa.2017.10.006_b0185) 2007; 43
Collombet (10.1016/j.compositesa.2017.10.006_b0055) 1998; 58
10.1016/j.compositesa.2017.10.006_b0120
10.1016/j.compositesa.2017.10.006_b0165
Allison (10.1016/j.compositesa.2017.10.006_b0030) 2006; 58
Geubelle (10.1016/j.compositesa.2017.10.006_b0060) 1998; 29
Ming-Yuan (10.1016/j.compositesa.2017.10.006_b0260) 1989; 25
Bouvet (10.1016/j.compositesa.2017.10.006_b0110) 2012; 72
Zheng (10.1016/j.compositesa.2017.10.006_b0140) 1995; 53
Rybicki (10.1016/j.compositesa.2017.10.006_b0065) 1977; 9
O’Brien (10.1016/j.compositesa.2017.10.006_b0045) 1982; 775
Benzeggagh (10.1016/j.compositesa.2017.10.006_b0195) 1996; 56
Van der Meer (10.1016/j.compositesa.2017.10.006_b0105) 2012; 46
References_xml – volume: 126
  start-page: 196
  year: 2015
  end-page: 206
  ident: b0155
  article-title: An enriched shell element formulation for efficient modeling of multiple delamination propagation in laminates
  publication-title: Compos Struct
  contributor:
    fullname: Fagerström
– volume: 88
  start-page: 749
  year: 2011
  end-page: 773
  ident: b0090
  article-title: Mesh-independent matrix cracking and delamination modeling in laminated composites
  publication-title: Int J Numer Meth Eng
  contributor:
    fullname: Dávila
– volume: 165
  start-page: 77
  year: 2010
  end-page: 92
  ident: b0100
  article-title: The evolution of a transverse intra-ply crack coupled to delamination cracks
  publication-title: Int J Fract
  contributor:
    fullname: Yang
– volume: 127
  start-page: 104
  year: 2014
  end-page: 134
  ident: b0175
  article-title: A floating node method for the modelling of discontinuities in composites
  publication-title: Eng Fract Mech
  contributor:
    fullname: Tay
– volume: 108
  start-page: 161
  year: 2014
  end-page: 171
  ident: b0085
  article-title: Finite element modelling of damage induced by low-velocity impact on composite laminates
  publication-title: Compos Struct
  contributor:
    fullname: Aymerich
– volume: 32
  start-page: 25
  year: 2001
  end-page: 44
  ident: b0115
  article-title: A shell/3D modeling technique for the analysis of delaminated composite laminates
  publication-title: Compos Part A: Appl Sci Manuf
  contributor:
    fullname: O’Brien
– volume: 46
  start-page: 603
  year: 2012
  end-page: 623
  ident: b0105
  article-title: Computational modeling of complex failure mechanisms in laminates
  publication-title: J Compos Mater
  contributor:
    fullname: Wisnom
– volume: 257
  start-page: 395
  year: 2004
  end-page: 407
  ident: b0245
  article-title: Coefficient of friction and wear of a carbon fiber epoxy matrix composite
  publication-title: Wear
  contributor:
    fullname: Schön
– volume: 167
  start-page: 88
  year: 2017
  end-page: 95
  ident: b0170
  article-title: Use of an enriched shell finite element to simulate delamination-migration in a composite laminate
  publication-title: Compos Struct
  contributor:
    fullname: McElroy
– volume: 79
  start-page: 192
  year: 2015
  end-page: 202
  ident: b0210
  article-title: Simulation of delamination-migration and core crushing in a CFRP sandwich structure
  publication-title: Compos Part A: Appl Sci Manuf
  contributor:
    fullname: Yuan
– volume: 25
  start-page: 1053
  year: 1989
  end-page: 1067
  ident: b0260
  article-title: Crack deflection at an interface between dissimilar elastic materials
  publication-title: Int J Solids Struct
  contributor:
    fullname: Hutchinson
– volume: 94
  start-page: 3364
  year: 2012
  end-page: 3378
  ident: b0075
  article-title: Simulation of drop-weight impact and compression after impact tests on composite laminates
  publication-title: Compos Struct
  contributor:
    fullname: Mayugo
– volume: 43
  start-page: 9
  year: 2007
  end-page: 28
  ident: b0185
  article-title: Development of a finite-element analysis methodology for the propagation of delaminations in composite structures
  publication-title: Mech Compos Mater
  contributor:
    fullname: Bayandor
– volume: 67
  start-page: 2715
  year: 2007
  end-page: 2727
  ident: b0230
  article-title: Prediction of size effects in notched laminates using continuum damage mechanics
  publication-title: Compos Sci Technol
  contributor:
    fullname: Dávila
– volume: 103
  start-page: 314
  year: 2017
  end-page: 326
  ident: b0005
  article-title: Interaction of delaminations and matrix cracks in a CFRP plate, part I: a test method for model validation
  publication-title: Compos Part A: Appl Sci Manuf
  contributor:
    fullname: Pankow
– volume: 51
  start-page: 936
  year: 2013
  end-page: 945
  ident: b0095
  article-title: Strength prediction in open hole composite laminates by using discrete damage modeling
  publication-title: AIAA J
  contributor:
    fullname: Hallett
– volume: 63
  start-page: 15
  year: 2011
  ident: b0025
  article-title: Integrated computational materials engineering: a perspective on progress and future steps
  publication-title: JOM: J Miner, Metals Mater Soc
  contributor:
    fullname: Allison
– volume: 9
  start-page: 931
  year: 1977
  end-page: 938
  ident: b0065
  article-title: A finite element calculation of stress intensity factors by a modified crack closure integral
  publication-title: Eng Fract Mech
  contributor:
    fullname: Kanninen
– volume: 36
  start-page: 221
  year: 1997
  end-page: 247
  ident: b0240
  article-title: Investigations of delamination criticality and the transferability of growth criteria
  publication-title: Compos Struct
  contributor:
    fullname: Nilsson
– volume: 36
  start-page: 1182
  year: 2009
  end-page: 1193
  ident: b0125
  article-title: Low velocity impact on CFRP plates with compressive preload: test and modelling
  publication-title: Int J Impact Eng
  contributor:
    fullname: Weiße
– volume: 136
  start-page: 616
  year: 2016
  end-page: 625
  ident: b0160
  article-title: An enriched shell element formulation for modeling of inter- and intralaminar crack propagation in laminates
  publication-title: Compos Struct
  contributor:
    fullname: Svenning
– volume: 94
  start-page: 2902
  year: 2012
  end-page: 2913
  ident: b0080
  article-title: Modelling damage evolution in composite laminates subjected to low velocity impact
  publication-title: Compos Struct
  contributor:
    fullname: Soutis
– volume: 5
  start-page: 277
  year: 1995
  end-page: 296
  ident: b0190
  article-title: Composite skin-stiffener debond analyses using fracture mechanics approach with shell elements
  publication-title: Compos Eng
  contributor:
    fullname: Sleight
– volume: 71
  start-page: 192
  year: 2015
  end-page: 203
  ident: b0200
  article-title: Modeling delamination migration in cross-ply tape laminates
  publication-title: Compos Part A: Appl Sci Manuf
  contributor:
    fullname: Tay
– volume: 56
  start-page: 439
  year: 1996
  end-page: 449
  ident: b0195
  article-title: Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus
  publication-title: Compos Sci Technol
  contributor:
    fullname: Kenane
– volume: 193
  start-page: 3173
  year: 2004
  end-page: 3194
  ident: b0145
  article-title: A discontinuous shell-interface element for delamination analysis of laminated composite structures
  publication-title: Comp Meth Appl Mech Eng
  contributor:
    fullname: Larsson
– start-page: 2
  year: 2004
  end-page: 28
  ident: b0010
  article-title: The world-wide failure exercise: Its origin, concept and content
  publication-title: Failure criteria in fiber reinforced polymer composites: the world wide failure exercise
  contributor:
    fullname: Soden
– volume: 133
  start-page: 041010
  year: 2011
  ident: b0130
  article-title: Augmented cohesive elements for efficient delamination analyses of composite laminates
  publication-title: J Eng Mater Technol
  contributor:
    fullname: Lua
– volume: 46
  start-page: 2313
  year: 2012
  end-page: 2341
  ident: b0220
  article-title: Material and structural response of polymer-matrix fibre-reinforced composites
  publication-title: J Compos Mater
  contributor:
    fullname: Camanho
– volume: 775
  start-page: 140
  year: 1982
  end-page: 167
  ident: b0045
  article-title: Characterization of delamination onset and growth in a composite laminate
  publication-title: Dam Compos Mater, ASTM STP
  contributor:
    fullname: O’Brien
– volume: 58
  start-page: 25
  year: 2006
  end-page: 27
  ident: b0030
  article-title: Integrated computational materials engineering: a new paradigm for the global materials profession
  publication-title: JOM: J Miner, Metals Mater Soc
  contributor:
    fullname: Christodoulou
– volume: 11
  start-page: 470
  year: 1977
  end-page: 487
  ident: b0040
  article-title: An energy release rate approach for stable crack growth in the free-edge delamination problem
  publication-title: J Compos Mater
  contributor:
    fullname: Fox
– volume: 54
  start-page: 79
  year: 2013
  end-page: 87
  ident: b0225
  article-title: Delamination growth directionality and the subsequent migration processes–the key to damage tolerant design
  publication-title: Compos Part A: Appl Sci Manuf
  contributor:
    fullname: Ankersen
– volume: 41
  start-page: 795
  year: 2010
  end-page: 805
  ident: b0070
  article-title: Modelling discrete failures in composites with interface elements
  publication-title: Compos Part A: Appl Sci Manuf
  contributor:
    fullname: Wisnom
– volume: 105
  start-page: 102
  year: 2014
  end-page: 109
  ident: b0215
  article-title: The relationship between mixed-mode II/III delamination and delamination migration in composite laminates
  publication-title: Compos Sci Technol
  contributor:
    fullname: Pinho
– volume: 60
  start-page: 9
  year: 2008
  end-page: 10
  ident: b0035
  article-title: Integrated computational materials engineering (ICME): a mode for the future?
  publication-title: JOM: J Miner, Metals Mater Soc
  contributor:
    fullname: Apelian
– volume: 29
  start-page: 589
  year: 1998
  end-page: 602
  ident: b0060
  article-title: Impact-induced delamination of composites: a 2D simulation
  publication-title: Compos Part B: Eng
  contributor:
    fullname: Baylor
– volume: 140
  start-page: 602
  year: 2016
  end-page: 611
  ident: b0255
  article-title: Assessment of two methods for the accurate prediction of transverse stress distributions in laminates
  publication-title: Compos Struct
  contributor:
    fullname: Fagerström
– volume: 72
  start-page: 1977
  year: 2012
  end-page: 1988
  ident: b0110
  article-title: Low velocity impact modeling in composite laminates capturing permanent indentation
  publication-title: Compos Sci Technol
  contributor:
    fullname: Barrau
– volume: 45
  start-page: 663
  year: 2008
  end-page: 672
  ident: b0135
  article-title: Effective simulation of delamination in aeronautical structures using shells and cohesive elements
  publication-title: J Aircraft
  contributor:
    fullname: Turon
– volume: 58
  start-page: 463
  year: 1998
  end-page: 478
  ident: b0055
  article-title: Impact behavior of laminated composites: physical basis for finite element analysis
  publication-title: Compos Sci Technol
  contributor:
    fullname: Lataillade
– volume: 53
  start-page: 111
  year: 1995
  end-page: 118
  ident: b0140
  article-title: A double-plate finite-element model for the impact-induced delamination problem
  publication-title: Compos Sci Technol
  contributor:
    fullname: Sun
– volume: 47
  start-page: 2417
  year: 2013
  end-page: 2426
  ident: b0015
  article-title: The background to the third world-wide failure exercise
  publication-title: J Compos Mater
  contributor:
    fullname: Li
– volume: 58
  start-page: 463
  issue: 3
  year: 1998
  ident: 10.1016/j.compositesa.2017.10.006_b0055
  article-title: Impact behavior of laminated composites: physical basis for finite element analysis
  publication-title: Compos Sci Technol
  doi: 10.1016/S0266-3538(97)00146-2
  contributor:
    fullname: Collombet
– volume: 71
  start-page: 192
  year: 2015
  ident: 10.1016/j.compositesa.2017.10.006_b0200
  article-title: Modeling delamination migration in cross-ply tape laminates
  publication-title: Compos Part A: Appl Sci Manuf
  doi: 10.1016/j.compositesa.2015.01.021
  contributor:
    fullname: De Carvalho
– volume: 94
  start-page: 3364
  issue: 11
  year: 2012
  ident: 10.1016/j.compositesa.2017.10.006_b0075
  article-title: Simulation of drop-weight impact and compression after impact tests on composite laminates
  publication-title: Compos Struct
  doi: 10.1016/j.compstruct.2012.05.015
  contributor:
    fullname: González
– ident: 10.1016/j.compositesa.2017.10.006_b0180
– volume: 41
  start-page: 795
  issue: 7
  year: 2010
  ident: 10.1016/j.compositesa.2017.10.006_b0070
  article-title: Modelling discrete failures in composites with interface elements
  publication-title: Compos Part A: Appl Sci Manuf
  doi: 10.1016/j.compositesa.2010.02.011
  contributor:
    fullname: Wisnom
– ident: 10.1016/j.compositesa.2017.10.006_b0235
– ident: 10.1016/j.compositesa.2017.10.006_b0250
– volume: 193
  start-page: 3173
  issue: 30
  year: 2004
  ident: 10.1016/j.compositesa.2017.10.006_b0145
  article-title: A discontinuous shell-interface element for delamination analysis of laminated composite structures
  publication-title: Comp Meth Appl Mech Eng
  doi: 10.1016/j.cma.2003.08.009
  contributor:
    fullname: Larsson
– volume: 103
  start-page: 314
  year: 2017
  ident: 10.1016/j.compositesa.2017.10.006_b0005
  article-title: Interaction of delaminations and matrix cracks in a CFRP plate, part I: a test method for model validation
  publication-title: Compos Part A: Appl Sci Manuf
  doi: 10.1016/j.compositesa.2017.09.011
  contributor:
    fullname: McElroy
– volume: 167
  start-page: 88
  year: 2017
  ident: 10.1016/j.compositesa.2017.10.006_b0170
  article-title: Use of an enriched shell finite element to simulate delamination-migration in a composite laminate
  publication-title: Compos Struct
  doi: 10.1016/j.compstruct.2017.01.057
  contributor:
    fullname: McElroy
– volume: 56
  start-page: 439
  issue: 4
  year: 1996
  ident: 10.1016/j.compositesa.2017.10.006_b0195
  article-title: Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus
  publication-title: Compos Sci Technol
  doi: 10.1016/0266-3538(96)00005-X
  contributor:
    fullname: Benzeggagh
– volume: 127
  start-page: 104
  year: 2014
  ident: 10.1016/j.compositesa.2017.10.006_b0175
  article-title: A floating node method for the modelling of discontinuities in composites
  publication-title: Eng Fract Mech
  doi: 10.1016/j.engfracmech.2014.05.018
  contributor:
    fullname: Chen
– volume: 47
  start-page: 2417
  issue: 20–21
  year: 2013
  ident: 10.1016/j.compositesa.2017.10.006_b0015
  article-title: The background to the third world-wide failure exercise
  publication-title: J Compos Mater
  doi: 10.1177/0021998313499475
  contributor:
    fullname: Kaddour
– volume: 63
  start-page: 15
  issue: 4
  year: 2011
  ident: 10.1016/j.compositesa.2017.10.006_b0025
  article-title: Integrated computational materials engineering: a perspective on progress and future steps
  publication-title: JOM: J Miner, Metals Mater Soc
  doi: 10.1007/s11837-011-0053-y
  contributor:
    fullname: Allison
– volume: 67
  start-page: 2715
  issue: 13
  year: 2007
  ident: 10.1016/j.compositesa.2017.10.006_b0230
  article-title: Prediction of size effects in notched laminates using continuum damage mechanics
  publication-title: Compos Sci Technol
  doi: 10.1016/j.compscitech.2007.02.005
  contributor:
    fullname: Camanho
– volume: 9
  start-page: 931
  issue: 4
  year: 1977
  ident: 10.1016/j.compositesa.2017.10.006_b0065
  article-title: A finite element calculation of stress intensity factors by a modified crack closure integral
  publication-title: Eng Fract Mech
  doi: 10.1016/0013-7944(77)90013-3
  contributor:
    fullname: Rybicki
– volume: 105
  start-page: 102
  year: 2014
  ident: 10.1016/j.compositesa.2017.10.006_b0215
  article-title: The relationship between mixed-mode II/III delamination and delamination migration in composite laminates
  publication-title: Compos Sci Technol
  doi: 10.1016/j.compscitech.2014.10.001
  contributor:
    fullname: Canturri
– ident: 10.1016/j.compositesa.2017.10.006_b0050
– start-page: 2
  year: 2004
  ident: 10.1016/j.compositesa.2017.10.006_b0010
  article-title: The world-wide failure exercise: Its origin, concept and content
  contributor:
    fullname: Hinton
– volume: 46
  start-page: 2313
  issue: 19–20
  year: 2012
  ident: 10.1016/j.compositesa.2017.10.006_b0220
  article-title: Material and structural response of polymer-matrix fibre-reinforced composites
  publication-title: J Compos Mater
  doi: 10.1177/0021998312454478
  contributor:
    fullname: Pinho
– volume: 94
  start-page: 2902
  issue: 9
  year: 2012
  ident: 10.1016/j.compositesa.2017.10.006_b0080
  article-title: Modelling damage evolution in composite laminates subjected to low velocity impact
  publication-title: Compos Struct
  doi: 10.1016/j.compstruct.2012.03.039
  contributor:
    fullname: Shi
– volume: 79
  start-page: 192
  year: 2015
  ident: 10.1016/j.compositesa.2017.10.006_b0210
  article-title: Simulation of delamination-migration and core crushing in a CFRP sandwich structure
  publication-title: Compos Part A: Appl Sci Manuf
  doi: 10.1016/j.compositesa.2015.08.026
  contributor:
    fullname: McElroy
– volume: 25
  start-page: 1053
  issue: 9
  year: 1989
  ident: 10.1016/j.compositesa.2017.10.006_b0260
  article-title: Crack deflection at an interface between dissimilar elastic materials
  publication-title: Int J Solids Struct
  doi: 10.1016/0020-7683(89)90021-8
  contributor:
    fullname: Ming-Yuan
– volume: 5
  start-page: 277
  issue: 3
  year: 1995
  ident: 10.1016/j.compositesa.2017.10.006_b0190
  article-title: Composite skin-stiffener debond analyses using fracture mechanics approach with shell elements
  publication-title: Compos Eng
  doi: 10.1016/0961-9526(94)00097-S
  contributor:
    fullname: Wang
– volume: 60
  start-page: 9
  issue: 7
  year: 2008
  ident: 10.1016/j.compositesa.2017.10.006_b0035
  article-title: Integrated computational materials engineering (ICME): a mode for the future?
  publication-title: JOM: J Miner, Metals Mater Soc
  doi: 10.1007/s11837-008-0081-4
  contributor:
    fullname: Apelian
– volume: 108
  start-page: 161
  year: 2014
  ident: 10.1016/j.compositesa.2017.10.006_b0085
  article-title: Finite element modelling of damage induced by low-velocity impact on composite laminates
  publication-title: Compos Struct
  doi: 10.1016/j.compstruct.2013.09.004
  contributor:
    fullname: Feng
– ident: 10.1016/j.compositesa.2017.10.006_b0120
– volume: 257
  start-page: 395
  issue: 3
  year: 2004
  ident: 10.1016/j.compositesa.2017.10.006_b0245
  article-title: Coefficient of friction and wear of a carbon fiber epoxy matrix composite
  publication-title: Wear
  doi: 10.1016/j.wear.2004.01.008
  contributor:
    fullname: Schön
– volume: 58
  start-page: 25
  issue: 11
  year: 2006
  ident: 10.1016/j.compositesa.2017.10.006_b0030
  article-title: Integrated computational materials engineering: a new paradigm for the global materials profession
  publication-title: JOM: J Miner, Metals Mater Soc
  doi: 10.1007/s11837-006-0223-5
  contributor:
    fullname: Allison
– volume: 11
  start-page: 470
  issue: 4
  year: 1977
  ident: 10.1016/j.compositesa.2017.10.006_b0040
  article-title: An energy release rate approach for stable crack growth in the free-edge delamination problem
  publication-title: J Compos Mater
  doi: 10.1177/002199837701100409
  contributor:
    fullname: Rybicki
– volume: 133
  start-page: 041010
  issue: 4
  year: 2011
  ident: 10.1016/j.compositesa.2017.10.006_b0130
  article-title: Augmented cohesive elements for efficient delamination analyses of composite laminates
  publication-title: J Eng Mater Technol
  doi: 10.1115/1.4004694
  contributor:
    fullname: Qiao
– volume: 46
  start-page: 603
  issue: 5
  year: 2012
  ident: 10.1016/j.compositesa.2017.10.006_b0105
  article-title: Computational modeling of complex failure mechanisms in laminates
  publication-title: J Compos Mater
  doi: 10.1177/0021998311410473
  contributor:
    fullname: Van der Meer
– volume: 136
  start-page: 616
  year: 2016
  ident: 10.1016/j.compositesa.2017.10.006_b0160
  article-title: An enriched shell element formulation for modeling of inter- and intralaminar crack propagation in laminates
  publication-title: Compos Struct
  doi: 10.1016/j.compstruct.2015.10.028
  contributor:
    fullname: Brouzoulis
– volume: 53
  start-page: 111
  issue: 1
  year: 1995
  ident: 10.1016/j.compositesa.2017.10.006_b0140
  article-title: A double-plate finite-element model for the impact-induced delamination problem
  publication-title: Compos Sci Technol
  doi: 10.1016/0266-3538(94)00079-4
  contributor:
    fullname: Zheng
– volume: 54
  start-page: 79
  year: 2013
  ident: 10.1016/j.compositesa.2017.10.006_b0225
  article-title: Delamination growth directionality and the subsequent migration processes–the key to damage tolerant design
  publication-title: Compos Part A: Appl Sci Manuf
  doi: 10.1016/j.compositesa.2013.07.004
  contributor:
    fullname: Canturri
– volume: 140
  start-page: 602
  year: 2016
  ident: 10.1016/j.compositesa.2017.10.006_b0255
  article-title: Assessment of two methods for the accurate prediction of transverse stress distributions in laminates
  publication-title: Compos Struct
  doi: 10.1016/j.compstruct.2015.12.036
  contributor:
    fullname: Främby
– volume: 88
  start-page: 749
  issue: 8
  year: 2011
  ident: 10.1016/j.compositesa.2017.10.006_b0090
  article-title: Mesh-independent matrix cracking and delamination modeling in laminated composites
  publication-title: Int J Numer Meth Eng
  doi: 10.1002/nme.3195
  contributor:
    fullname: Iarve
– ident: 10.1016/j.compositesa.2017.10.006_b0020
– ident: 10.1016/j.compositesa.2017.10.006_b0150
– volume: 126
  start-page: 196
  year: 2015
  ident: 10.1016/j.compositesa.2017.10.006_b0155
  article-title: An enriched shell element formulation for efficient modeling of multiple delamination propagation in laminates
  publication-title: Compos Struct
  doi: 10.1016/j.compstruct.2015.02.055
  contributor:
    fullname: Brouzoulis
– volume: 45
  start-page: 663
  issue: 2
  year: 2008
  ident: 10.1016/j.compositesa.2017.10.006_b0135
  article-title: Effective simulation of delamination in aeronautical structures using shells and cohesive elements
  publication-title: J Aircraft
  doi: 10.2514/1.32832
  contributor:
    fullname: Dávila
– volume: 72
  start-page: 1977
  issue: 16
  year: 2012
  ident: 10.1016/j.compositesa.2017.10.006_b0110
  article-title: Low velocity impact modeling in composite laminates capturing permanent indentation
  publication-title: Compos Sci Technol
  doi: 10.1016/j.compscitech.2012.08.019
  contributor:
    fullname: Bouvet
– volume: 36
  start-page: 1182
  issue: 10
  year: 2009
  ident: 10.1016/j.compositesa.2017.10.006_b0125
  article-title: Low velocity impact on CFRP plates with compressive preload: test and modelling
  publication-title: Int J Impact Eng
  doi: 10.1016/j.ijimpeng.2009.04.006
  contributor:
    fullname: Heimbs
– volume: 43
  start-page: 9
  issue: 1
  year: 2007
  ident: 10.1016/j.compositesa.2017.10.006_b0185
  article-title: Development of a finite-element analysis methodology for the propagation of delaminations in composite structures
  publication-title: Mech Compos Mater
  doi: 10.1007/s11029-007-0002-6
  contributor:
    fullname: Orifici
– ident: 10.1016/j.compositesa.2017.10.006_b0165
– volume: 32
  start-page: 25
  issue: 1
  year: 2001
  ident: 10.1016/j.compositesa.2017.10.006_b0115
  article-title: A shell/3D modeling technique for the analysis of delaminated composite laminates
  publication-title: Compos Part A: Appl Sci Manuf
  doi: 10.1016/S1359-835X(00)00133-0
  contributor:
    fullname: Krueger
– volume: 775
  start-page: 140
  issue: 2
  year: 1982
  ident: 10.1016/j.compositesa.2017.10.006_b0045
  article-title: Characterization of delamination onset and growth in a composite laminate
  publication-title: Dam Compos Mater, ASTM STP
  contributor:
    fullname: O’Brien
– volume: 165
  start-page: 77
  issue: 1
  year: 2010
  ident: 10.1016/j.compositesa.2017.10.006_b0100
  article-title: The evolution of a transverse intra-ply crack coupled to delamination cracks
  publication-title: Int J Fract
  doi: 10.1007/s10704-010-9506-5
  contributor:
    fullname: Zhou
– volume: 29
  start-page: 589
  issue: 5
  year: 1998
  ident: 10.1016/j.compositesa.2017.10.006_b0060
  article-title: Impact-induced delamination of composites: a 2D simulation
  publication-title: Compos Part B: Eng
  doi: 10.1016/S1359-8368(98)00013-4
  contributor:
    fullname: Geubelle
– volume: 51
  start-page: 936
  issue: 4
  year: 2013
  ident: 10.1016/j.compositesa.2017.10.006_b0095
  article-title: Strength prediction in open hole composite laminates by using discrete damage modeling
  publication-title: AIAA J
  doi: 10.2514/1.J051773
  contributor:
    fullname: Swindeman
– volume: 36
  start-page: 221
  year: 1997
  ident: 10.1016/j.compositesa.2017.10.006_b0240
  article-title: Investigations of delamination criticality and the transferability of growth criteria
  publication-title: Compos Struct
  doi: 10.1016/S0263-8223(96)00079-7
  contributor:
    fullname: Olsson
– ident: 10.1016/j.compositesa.2017.10.006_b0205
SSID ssj0003391
Score 2.3596127
Snippet Numerical simulations are presented of a recently developed test which creates multiple delaminations in a CFRP laminate specimen that grow and interact via...
SourceID pubmedcentral
proquest
crossref
pubmed
nasa
elsevier
SourceType Open Access Repository
Aggregation Database
Index Database
Publisher
StartPage 252
SubjectTerms A. Laminates
B. Delamination
C. Fracture
Composite Materials
D. Finite element analysis (FEA)
Structural Mechanics
Title Interaction of delaminations and matrix cracks in a CFRP plate, Part II: Simulation using an enriched shell finite element model
URI https://dx.doi.org/10.1016/j.compositesa.2017.10.006
https://ntrs.nasa.gov/citations/20190025754
https://www.ncbi.nlm.nih.gov/pubmed/33479561
https://search.proquest.com/docview/2480335767
https://pubmed.ncbi.nlm.nih.gov/PMC7816820
Volume 103
hasFullText 1
inHoldings 1
isFullTextHit
isPrint
link http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwpV1da9RAFB1KBdEH8aNq_Ci34KPpJplJZiK-lMVlV7EUa2HfwmQ-asRml-4WfBJ_uvdmknZXFAQfk0wguedm5kzm3DOMvVIexxDFTax0LmOhpYlLb8tYGZ9JjwRbdBVyH4-L6Zl4P8_nO2w81MKQrLLv-0Of3vXW_ZlRH83RsmlGpymZz_F8nkrqhgXN28lsC3P68MeNzIPzMky66HcXtr7NDm40XiTbJm2UW5EFUSoPg9Drb2PUbqtX-k9U9HdF5cYQNbnP7vXcEo7C4z9gO659yO5uOA4-Yj-7P4ChmAEWHsgjksQwXfaBbi1ckGf_dzCXVHwPTQsaxpNPJ7D8hqz0NZxgcGA2ewOnzUW_8xeQdv4cbwbMRVKWWliRvBR8Q4QWXFCoQ7fpzh47m7z7PJ7G_SYMscllso5z6XmaJdYVuXDKWIxw7k0qam8KpTUiqjQ3JS3fZGVdYkKkLqktsqrU4VTE8scYtkXrnjKQ3BamkIkX3Itae82t4T7NnLKalmMjlg1hr5bBa6MaRGhfqw2sKsKKLiFWEXs7AFRtJU6FY8K_3L5HoFYI24rOl0QCZS4idjCgXOEHR6sounWLK2wkFCYVTtNkxJ4E1K-fllNdLjLSiMmtfLhuQGbe21fa5ktn6i1pA5QsefZ_r_Oc3aGjoLd5wXbXl1fuJbKmdb3ffRb77NbR7MP0-BeVwxno
link.rule.ids 230,315,783,787,888,4511,24130,27938,27939,45599,45693
linkProvider Elsevier
linkToHtml http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwpV1ba9swFBalhV0exi5d511PYY9zY1uyJZe-jLCQbG0pawt5M7Ium8fqhCaFPo399J3jS5uMDQZ7tWSQ9R1Ln6TvfGLsrfI4hyhuQqVTGQotTZh7m4fK-ER6JNiiyZA7Os7G5-LjNJ1usGGfC0Oyym7sb8f0ZrTungy63hzMq2pwGpP5HE-nsaRhWOC6fUuQfxYG9d6PW50H53m76qL9Lqx-h-3eirxIt03iKLcgD6JY7rVKr79NUpu1Xug_cdHfJZUrc9ToIXvQkUt437b_Edtw9WN2f8Vy8An72WwBttkMMPNAJpGkhmnCD3Rt4YJM-6_BXFL2PVQ1aBiOPp_A_DvS0ndwgr0Dk8k-nFYX3dVfQOL5L_gyYDCStNTCgvSl4CtitOBaiTo0t-5ss_PRh7PhOOxuYQhNKqNlmErP4ySyLkuFU8YiQ0u9iUXpTaa0RkiV5ian85skL3OMiNhFpUVaFTtci1j-FLttVrtnDCS3mclk5AX3otRec2u4jxOnrKbz2IAlfbcX89Zso-hVaN-KFawKwoqKEKuAHfQAFWuRU-Ck8C-vbxOoBcK2oOc5sUCZioDt9igX-MfRMYqu3ewKKwmFQYXrNBmwnRb1m9ZySsxFShowuRYPNxXIzXu9pK6-Nq7ekm5ASaLn__c5b9jd8dnRYXE4Of70gt2jklZ885JtLi-v3CukUMvydfOL_AIUdxuK
openUrl ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Ajournal&rft.genre=article&rft.atitle=Interaction+of+delaminations+and+matrix+cracks+in+a+CFRP+plate%2C+Part+II%3A+Simulation+using+an+enriched+shell+finite+element+model&rft.jtitle=Composites.+Part+A%2C+Applied+science+and+manufacturing&rft.au=McElroy%2C+Mark+W.&rft.au=Gutkin%2C+Renaud&rft.au=Pankow%2C+Mark&rft.date=2017-12-01&rft.pub=Elsevier+Ltd&rft.issn=1359-835X&rft.eissn=1878-5840&rft.volume=103&rft.spage=252&rft.epage=262&rft_id=info:doi/10.1016%2Fj.compositesa.2017.10.006&rft.externalDocID=S1359835X17303640
thumbnail_l http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=1359-835X&client=summon
thumbnail_m http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=1359-835X&client=summon
thumbnail_s http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=1359-835X&client=summon