A comparison of the predictive capabilities of current failure theories for composite laminates: additional contributions
Following the publication of an article by Soden, Hinton and Kaddour (Compos Sci Technol, V58, pp. 1225–54, 1998), which compared the predictions of 14 internationally recognised failure theories for fibre reinforced polymer composite laminates, the present paper extends that comparative study to in...
Saved in:
Published in | Composites science and technology Vol. 64; no. 3; pp. 449 - 476 |
---|---|
Main Authors | , , |
Format | Journal Article |
Language | English |
Published |
Elsevier Ltd
01.03.2004
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Abstract | Following the publication of an article by Soden, Hinton and Kaddour (Compos Sci Technol, V58, pp. 1225–54, 1998), which compared the predictions of 14 internationally recognised failure theories for fibre reinforced polymer composite laminates, the present paper extends that comparative study to include five more theories, supplied by their originators. Evaluation of the predictive capabilities of the additional theories was carried out in an identical manner to the original study. The same test cases were utilised, covering a wide range of lay-ups, materials and in-plane loading conditions. The results (initial and final failure envelopes and representative stress–strain curves) have been superimposed to show similarities and differences between the predictions of the 19 theories. Final failure predictions for the additional theories fall within the existing range obtained from the original 14 theories but the initial failure predictions for the additional theories have widened the previously observed range. Comments are provided on the possible reasons for the increased spread. |
---|---|
AbstractList | Following the publication of an article by Soden, Hinton and Kaddour (Compos Sci Technol, V58, pp. 1225–54, 1998), which compared the predictions of 14 internationally recognised failure theories for fibre reinforced polymer composite laminates, the present paper extends that comparative study to include five more theories, supplied by their originators. Evaluation of the predictive capabilities of the additional theories was carried out in an identical manner to the original study. The same test cases were utilised, covering a wide range of lay-ups, materials and in-plane loading conditions. The results (initial and final failure envelopes and representative stress–strain curves) have been superimposed to show similarities and differences between the predictions of the 19 theories. Final failure predictions for the additional theories fall within the existing range obtained from the original 14 theories but the initial failure predictions for the additional theories have widened the previously observed range. Comments are provided on the possible reasons for the increased spread. |
Author | Kaddour, A.S. Soden, P.D. Hinton, M.J. |
Author_xml | – sequence: 1 givenname: A.S. surname: Kaddour fullname: Kaddour, A.S. email: askaddour@qinetiq.com organization: QinetiQ FST, Farnborough, Hampshire, GV14 0LX UK – sequence: 2 givenname: M.J. surname: Hinton fullname: Hinton, M.J. email: mjhinton@qinetiq.com organization: QinetiQ Fort Halstead, Kent, TN14 7BP UK – sequence: 3 givenname: P.D. surname: Soden fullname: Soden, P.D. email: p.soden@umist.ac.uk organization: Mechanical Aerospace and Manufacturing Engineering Department, UMIST, UK |
BookMark | eNqFkEtLxDAUhYMoOD5-gtCV6KJ60zzauhERXyC4UNchydxipJPUJBXm39vOiFtX4XK-cyDfAdn1wSMhJxQuKFB5-QqVlCUTrDkDdg5QVbLkO2RBm7otKQjYJYs_ZJ8cpPQJALVoqwVZ3xQ2rAYdXQq-CF2RP7AYIi6dze4bC6sHbVzvssM0x3aMEX0uOu36MeKMhzhnXYibpZBcxqLXK-d1xnRV6OVyagev-yn3OTozzmc6Inud7hMe_76H5P3-7u32sXx-eXi6vXkuLQeey1YL0dXAWC1kLZrWyIa3aLgx0HLKUGpphQSDxphKWMM0cN02rJWmkk3H2CE53e4OMXyNmLJauWSx77XHMCZVNZTyuuETKLagjSGliJ0aolvpuFYU1CxabUSr2aICpjai1dy73vZw-sW3w6iSdejt5DCizWoZ3D8LP4WJiXw |
CitedBy_id | crossref_primary_10_1016_j_compscitech_2018_04_033 crossref_primary_10_1016_j_compstruc_2010_12_003 crossref_primary_10_1016_j_ress_2012_08_011 crossref_primary_10_1016_j_compstruct_2016_04_012 crossref_primary_10_1177_0021998312449889 crossref_primary_10_1016_j_mechmat_2008_05_004 crossref_primary_10_1007_s11837_012_0509_8 crossref_primary_10_1080_15376490902782223 crossref_primary_10_1016_j_compstruct_2020_112797 crossref_primary_10_1177_0021998312474044 crossref_primary_10_3390_ma17061387 crossref_primary_10_1016_j_oceaneng_2013_03_001 crossref_primary_10_1016_j_polymertesting_2017_04_010 crossref_primary_10_1115_1_3013822 crossref_primary_10_1016_j_polymertesting_2017_08_041 crossref_primary_10_1016_j_polymertesting_2016_12_023 crossref_primary_10_1177_0021998313484075 crossref_primary_10_1590_1679_78254301 crossref_primary_10_1016_j_procir_2017_03_365 crossref_primary_10_1016_S0266_3538_03_00227_6 crossref_primary_10_1016_j_compstruct_2020_113537 crossref_primary_10_1016_j_compositesb_2014_01_007 crossref_primary_10_1016_j_compositesb_2012_01_003 crossref_primary_10_1080_15376494_2020_1821265 crossref_primary_10_1016_j_compscitech_2021_109206 crossref_primary_10_1016_j_ijsolstr_2019_07_015 crossref_primary_10_1007_s10443_015_9456_1 crossref_primary_10_1007_s13272_016_0210_7 crossref_primary_10_1016_j_tws_2019_04_023 crossref_primary_10_1186_s40064_016_3726_8 crossref_primary_10_1002_pc_26867 crossref_primary_10_1016_j_oceaneng_2023_114993 crossref_primary_10_1007_s13272_020_00488_1 crossref_primary_10_1016_j_compstruc_2007_04_009 crossref_primary_10_1016_j_msea_2008_02_023 crossref_primary_10_1177_10567895211019065 crossref_primary_10_1115_1_2200654 crossref_primary_10_6089_jscm_48_77 crossref_primary_10_1177_0021998311432775 crossref_primary_10_1007_s11223_010_9209_1 crossref_primary_10_3390_ma11101919 crossref_primary_10_1007_s10010_008_0078_8 crossref_primary_10_1016_j_compstruct_2019_01_107 crossref_primary_10_1016_j_compositesb_2014_09_032 crossref_primary_10_1016_j_compscitech_2008_05_004 crossref_primary_10_1016_j_tws_2018_12_002 crossref_primary_10_1016_j_tws_2022_110425 crossref_primary_10_3390_ma12193133 crossref_primary_10_1080_15376494_2022_2129529 crossref_primary_10_1016_j_tws_2018_07_047 crossref_primary_10_1177_0021998317690917 crossref_primary_10_1007_s11029_018_9767_z crossref_primary_10_1016_j_compstruct_2020_113435 crossref_primary_10_1088_1361_651X_ab1f63 crossref_primary_10_1016_j_euromechsol_2015_10_006 crossref_primary_10_1016_j_compscitech_2019_01_012 crossref_primary_10_1088_2053_1591_ab10c9 crossref_primary_10_1155_2014_503483 crossref_primary_10_1177_0021998311401093 crossref_primary_10_1115_1_4065726 crossref_primary_10_1007_s12205_019_1988_8 crossref_primary_10_1016_j_cja_2019_10_009 crossref_primary_10_61653_joast_v67i4_2015_405 crossref_primary_10_1177_0731684409357257 crossref_primary_10_1007_s11668_019_00768_x crossref_primary_10_1007_s00158_012_0875_4 crossref_primary_10_1002_adma_201101683 crossref_primary_10_1016_j_compstruct_2014_11_011 crossref_primary_10_1016_j_ress_2012_05_006 crossref_primary_10_1016_j_compositesb_2018_11_101 crossref_primary_10_1007_s12206_020_0327_9 crossref_primary_10_1016_j_ast_2016_05_001 crossref_primary_10_1016_j_compositesb_2011_10_007 crossref_primary_10_1177_0021998312460261 crossref_primary_10_1016_j_compscitech_2019_02_004 crossref_primary_10_3744_SNAK_2015_52_2_143 crossref_primary_10_1016_j_compstruct_2008_07_023 crossref_primary_10_1051_matecconf_202032903048 crossref_primary_10_1177_0954405418763995 crossref_primary_10_2514_1_J057677 crossref_primary_10_1177_0021998313488809 crossref_primary_10_1177_0021998308093911 crossref_primary_10_1177_0731684407079753 crossref_primary_10_1002_pc_25059 crossref_primary_10_1016_j_compositesa_2004_11_012 crossref_primary_10_1177_0021998310387682 crossref_primary_10_1007_s00773_012_0205_y crossref_primary_10_1016_j_compositesa_2007_07_008 crossref_primary_10_1016_j_cja_2023_05_027 crossref_primary_10_1177_0021998312462616 crossref_primary_10_1016_j_jcomc_2020_100066 crossref_primary_10_1177_0021998313476328 crossref_primary_10_1016_j_compstruct_2023_117422 crossref_primary_10_1016_j_aej_2020_06_032 crossref_primary_10_1177_0021998311430544 crossref_primary_10_1177_0021998313494095 crossref_primary_10_1051_smdo_2008001 crossref_primary_10_1177_0021998312473346 |
Cites_doi | 10.1016/S0266-3538(97)00013-4 10.1016/S0266-3538(97)00191-7 10.1016/S0266-3538(97)00192-9 10.1016/S0266-3538(02)00125-2 10.1016/S0266-3538(97)00193-0 10.1016/S0266-3538(96)00140-6 10.1016/S0266-3538(98)00078-5 10.1016/S0266-3538(96)00143-1 10.1016/S0266-3538(96)00144-3 10.1016/S0266-3538(98)00077-3 10.1016/S0266-3538(96)00139-X 10.1016/S0266-3538(98)00074-8 10.1016/S0266-3538(02)00092-1 10.1016/S0266-3538(97)00014-6 10.1016/S0266-3538(96)00142-X 10.1016/S0266-3538(96)00141-8 10.1016/S0266-3538(96)00145-5 |
ContentType | Journal Article |
Copyright | 2003 QinetiQ Ltd |
Copyright_xml | – notice: 2003 QinetiQ Ltd |
DBID | AAYXX CITATION 7SR 8FD JG9 |
DOI | 10.1016/S0266-3538(03)00226-4 |
DatabaseName | CrossRef Engineered Materials Abstracts Technology Research Database Materials Research Database |
DatabaseTitle | CrossRef Materials Research Database Technology Research Database Engineered Materials Abstracts |
DatabaseTitleList | Materials Research Database |
DeliveryMethod | fulltext_linktorsrc |
Discipline | Economics Engineering |
EISSN | 1879-1050 |
EndPage | 476 |
ExternalDocumentID | 10_1016_S0266_3538_03_00226_4 S0266353803002264 |
GroupedDBID | --K --M .-4 .~1 0R~ 1B1 1~. 1~5 29F 4.4 457 4G. 5GY 5VS 6TJ 7-5 71M 8P~ 9JN AABNK AABXZ AACTN AAEDT AAEDW AAEPC AAIAV AAIKJ AAKOC AALRI AAOAW AAQFI AAQXK AAXUO ABFNM ABMAC ABXDB ABXRA ABYKQ ACDAQ ACGFS ACIWK ACNNM ACRLP ADBBV ADEZE ADIYS ADMUD ADTZH AEBSH AECPX AEKER AENEX AEZYN AFKWA AFRZQ AFTJW AGHFR AGUBO AGYEJ AHHHB AHJVU AI. AIEXJ AIKHN AITUG AJBFU AJOXV ALMA_UNASSIGNED_HOLDINGS AMFUW AMRAJ ASPBG AVWKF AXJTR AZFZN BJAXD BKOJK BLXMC CS3 DU5 EBS EFJIC EFLBG EJD EO8 EO9 EP2 EP3 F5P FDB FEDTE FGOYB FIRID FNPLU FYGXN G-2 G-Q GBLVA HVGLF HZ~ IHE J1W JJJVA KOM LY7 M24 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 SET SEW SMS SPC SPCBC SSM SST SSZ T5K T9H VH1 WUQ XPP ZMT ~G- AAXKI AAYXX AFJKZ AKRWK CITATION 7SR 8FD JG9 |
ID | FETCH-LOGICAL-c404t-9a55f70337567589b6849eb4bb09413e6a6c560bebbb25cb3a04a98396b268f33 |
IEDL.DBID | AIKHN |
ISSN | 0266-3538 |
IngestDate | Fri Oct 25 21:30:15 EDT 2024 Thu Sep 26 17:23:39 EDT 2024 Fri Feb 23 02:32:37 EST 2024 |
IsPeerReviewed | true |
IsScholarly | true |
Issue | 3 |
Keywords | Multiaxial failure envelopes Failure criteria B. Stress–strain curves |
Language | English |
LinkModel | DirectLink |
MergedId | FETCHMERGED-LOGICAL-c404t-9a55f70337567589b6849eb4bb09413e6a6c560bebbb25cb3a04a98396b268f33 |
Notes | ObjectType-Article-2 SourceType-Scholarly Journals-1 ObjectType-Feature-1 content type line 23 |
PQID | 28114784 |
PQPubID | 23500 |
PageCount | 28 |
ParticipantIDs | proquest_miscellaneous_28114784 crossref_primary_10_1016_S0266_3538_03_00226_4 elsevier_sciencedirect_doi_10_1016_S0266_3538_03_00226_4 |
PublicationCentury | 2000 |
PublicationDate | 2004-03-01 |
PublicationDateYYYYMMDD | 2004-03-01 |
PublicationDate_xml | – month: 03 year: 2004 text: 2004-03-01 day: 01 |
PublicationDecade | 2000 |
PublicationTitle | Composites science and technology |
PublicationYear | 2004 |
Publisher | Elsevier Ltd |
Publisher_xml | – name: Elsevier Ltd |
References | Hart-Smith (BIB8) 1998; 58 Gotsis, Chamis, Minnetyan (BIB3) 1998; 58 Hart-Smith (BIB7) 1998; 58 Hinton, Soden (BIB1) 1998; 58 Bogetti TA, Hoppel CPR, Harik VM, Newill JF, Burns BP. Predicting the nonlinear response and progressive failure of composite laminates. In this issue. Wolfe, Butalia (BIB13) 1998; 58 Huang ZM. A bridging model prediction of the tensile strength of composite laminates subjected to biaxial loads. In this issue. Cuntze RG, Freund A. The predictive capability of failure mode concept based strength criteria for multidirectional laminates. In this issue. Rotem (BIB10) 1998; 58 Sun, Tao (BIB11) 1998; 58 Zinoviev, Grigoriev, Labedeva, Tairova (BIB14) 1998; 58 Eckold (BIB4) 1998; 58 Soden, Hinton, Kaddour (BIB15) 1998; 58 McCartney (BIB6) 1998; 58 Hinton, Kaddour, Soden (BIB22) 2002; 62 Puck, Schürmann (BIB9) 1998; 58 Hinton MJ, Kaddour AS, Soden PD. Further assessment of the predictive capabilities of current failure theories for composite laminates: Comparison with experimental evidence. In this issue. Soden, Hinton, Kaddour (BIB2) 1998; 58 Mayes S, Hansen AC. Composite laminate failure analysis using multicontinuum theory. In this issue. Liu, Tsai (BIB12) 1998; 58 Hart-Smith (BIB16) 2002; 62 Edge (BIB5) 1998; 58 Wolfe (10.1016/S0266-3538(03)00226-4_BIB13) 1998; 58 10.1016/S0266-3538(03)00226-4_BIB17 10.1016/S0266-3538(03)00226-4_BIB18 Rotem (10.1016/S0266-3538(03)00226-4_BIB10) 1998; 58 Hinton (10.1016/S0266-3538(03)00226-4_BIB1) 1998; 58 McCartney (10.1016/S0266-3538(03)00226-4_BIB6) 1998; 58 Soden (10.1016/S0266-3538(03)00226-4_BIB15) 1998; 58 Hart-Smith (10.1016/S0266-3538(03)00226-4_BIB16) 2002; 62 10.1016/S0266-3538(03)00226-4_BIB19 Eckold (10.1016/S0266-3538(03)00226-4_BIB4) 1998; 58 Hinton (10.1016/S0266-3538(03)00226-4_BIB22) 2002; 62 Liu (10.1016/S0266-3538(03)00226-4_BIB12) 1998; 58 Zinoviev (10.1016/S0266-3538(03)00226-4_BIB14) 1998; 58 Puck (10.1016/S0266-3538(03)00226-4_BIB9) 1998; 58 Edge (10.1016/S0266-3538(03)00226-4_BIB5) 1998; 58 Hart-Smith (10.1016/S0266-3538(03)00226-4_BIB8) 1998; 58 Gotsis (10.1016/S0266-3538(03)00226-4_BIB3) 1998; 58 Soden (10.1016/S0266-3538(03)00226-4_BIB2) 1998; 58 10.1016/S0266-3538(03)00226-4_BIB20 Sun (10.1016/S0266-3538(03)00226-4_BIB11) 1998; 58 10.1016/S0266-3538(03)00226-4_BIB21 Hart-Smith (10.1016/S0266-3538(03)00226-4_BIB7) 1998; 58 |
References_xml | – volume: 58 start-page: 1125 year: 1998 end-page: 1136 ident: BIB11 article-title: Prediction of failure envelopes and stress strain behaviours of composite laminates publication-title: Compos Sci Tech. contributor: fullname: Tao – volume: 58 start-page: 1225 year: 1998 end-page: 1254 ident: BIB15 article-title: Comparison of the predictive capabilities of current failure theories for composite laminates publication-title: Compos Sci Tech. contributor: fullname: Kaddour – volume: 62 start-page: 1515 year: 2002 end-page: 1544 ident: BIB16 article-title: Expanding the capabilities of the ten-percent rule for predicting the strength of fibre-polymer composites publication-title: Compos Sci Tech. contributor: fullname: Hart-Smith – volume: 58 start-page: 1045 year: 1998 end-page: 1068 ident: BIB9 article-title: Failure analysis of FRP laminates by means of physically based phenomenological models publication-title: Compos Sci Tech. contributor: fullname: Schürmann – volume: 58 start-page: 1043 year: 1998 end-page: 1044 ident: BIB5 article-title: Stress based Grant-Sanders method for predicting failure of composite laminates publication-title: Compos Sci Tech. contributor: fullname: Edge – volume: 58 start-page: 1179 year: 1998 end-page: 1208 ident: BIB8 article-title: Predictions of a generalised maximum-shear-stress failure criterion for certain fibrous composite laminates publication-title: Compos Sci Tech. contributor: fullname: Hart-Smith – volume: 58 start-page: 1083 year: 1998 end-page: 1094 ident: BIB10 article-title: Prediction of laminate failure with Rotem failure criterion publication-title: Compos Sci Tech. contributor: fullname: Rotem – volume: 58 start-page: 1023 year: 1998 end-page: 1032 ident: BIB12 article-title: A progressive quadratic failure criterion of a laminate publication-title: Compos Sci Tech. contributor: fullname: Tsai – volume: 62 start-page: 1725 year: 2002 end-page: 1798 ident: BIB22 article-title: A comparison of the predictive capabilities of current failure theories for composite laminates, judged against experimental evidence publication-title: Compos Sci Tech. contributor: fullname: Soden – volume: 58 start-page: 1095 year: 1998 end-page: 1106 ident: BIB4 article-title: Failure criteria for use in the design environment publication-title: Compos Sci Tech. contributor: fullname: Eckold – volume: 58 start-page: 1001 year: 1998 end-page: 1010 ident: BIB1 article-title: Predicting failure in composite laminates publication-title: Compos Sci Tech. contributor: fullname: Soden – volume: 58 start-page: 1011 year: 1998 end-page: 1022 ident: BIB2 article-title: Lamina properties and lay-up configurations and loading conditions of a range fibre reinforced composite laminates publication-title: Compos Sci Tech. contributor: fullname: Kaddour – volume: 58 start-page: 1069 year: 1998 end-page: 1082 ident: BIB6 article-title: Predicting transverse crack formation in cross-ply laminate publication-title: Compos Sci Tech. contributor: fullname: McCartney – volume: 58 start-page: 1107 year: 1998 end-page: 1124 ident: BIB13 article-title: A strain energy based failure criterion for nonlinear analysis of composite laminates subjected to biaxial loading publication-title: Compos Sci Tech. contributor: fullname: Butalia – volume: 58 start-page: 1209 year: 1998 end-page: 1224 ident: BIB14 article-title: Strength of multilayered composites under plane stress state publication-title: Compos Sci Tech. contributor: fullname: Tairova – volume: 58 start-page: 1151 year: 1998 end-page: 1178 ident: BIB7 article-title: Predictions of the original and truncated maximum strain failure models for certain fibrous composite laminates publication-title: Compos Sci Tech. contributor: fullname: Hart-Smith – volume: 58 start-page: 1137 year: 1998 end-page: 1150 ident: BIB3 article-title: Prediction of composite laminate fracture publication-title: Compos Sci Tech. contributor: fullname: Minnetyan – volume: 58 start-page: 1125 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB11 article-title: Prediction of failure envelopes and stress strain behaviours of composite laminates publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(97)00013-4 contributor: fullname: Sun – volume: 58 start-page: 1209 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB14 article-title: Strength of multilayered composites under plane stress state publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(97)00191-7 contributor: fullname: Zinoviev – volume: 58 start-page: 1151 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB7 article-title: Predictions of the original and truncated maximum strain failure models for certain fibrous composite laminates publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(97)00192-9 contributor: fullname: Hart-Smith – volume: 62 start-page: 1725 year: 2002 ident: 10.1016/S0266-3538(03)00226-4_BIB22 article-title: A comparison of the predictive capabilities of current failure theories for composite laminates, judged against experimental evidence publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(02)00125-2 contributor: fullname: Hinton – volume: 58 start-page: 1179 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB8 article-title: Predictions of a generalised maximum-shear-stress failure criterion for certain fibrous composite laminates publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(97)00193-0 contributor: fullname: Hart-Smith – volume: 58 start-page: 1045 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB9 article-title: Failure analysis of FRP laminates by means of physically based phenomenological models publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(96)00140-6 contributor: fullname: Puck – volume: 58 start-page: 1011 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB2 article-title: Lamina properties and lay-up configurations and loading conditions of a range fibre reinforced composite laminates publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(98)00078-5 contributor: fullname: Soden – volume: 58 start-page: 1083 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB10 article-title: Prediction of laminate failure with Rotem failure criterion publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(96)00143-1 contributor: fullname: Rotem – volume: 58 start-page: 1095 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB4 article-title: Failure criteria for use in the design environment publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(96)00144-3 contributor: fullname: Eckold – volume: 58 start-page: 1225 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB15 article-title: Comparison of the predictive capabilities of current failure theories for composite laminates publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(98)00077-3 contributor: fullname: Soden – volume: 58 start-page: 1043 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB5 article-title: Stress based Grant-Sanders method for predicting failure of composite laminates publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(96)00139-X contributor: fullname: Edge – volume: 58 start-page: 1001 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB1 article-title: Predicting failure in composite laminates publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(98)00074-8 contributor: fullname: Hinton – ident: 10.1016/S0266-3538(03)00226-4_BIB19 – ident: 10.1016/S0266-3538(03)00226-4_BIB20 – volume: 62 start-page: 1515 year: 2002 ident: 10.1016/S0266-3538(03)00226-4_BIB16 article-title: Expanding the capabilities of the ten-percent rule for predicting the strength of fibre-polymer composites publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(02)00092-1 contributor: fullname: Hart-Smith – ident: 10.1016/S0266-3538(03)00226-4_BIB17 – ident: 10.1016/S0266-3538(03)00226-4_BIB18 – volume: 58 start-page: 1137 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB3 article-title: Prediction of composite laminate fracture publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(97)00014-6 contributor: fullname: Gotsis – volume: 58 start-page: 1069 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB6 article-title: Predicting transverse crack formation in cross-ply laminate publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(96)00142-X contributor: fullname: McCartney – volume: 58 start-page: 1023 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB12 article-title: A progressive quadratic failure criterion of a laminate publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(96)00141-8 contributor: fullname: Liu – ident: 10.1016/S0266-3538(03)00226-4_BIB21 – volume: 58 start-page: 1107 year: 1998 ident: 10.1016/S0266-3538(03)00226-4_BIB13 article-title: A strain energy based failure criterion for nonlinear analysis of composite laminates subjected to biaxial loading publication-title: Compos Sci Tech. doi: 10.1016/S0266-3538(96)00145-5 contributor: fullname: Wolfe |
SSID | ssj0007592 |
Score | 2.1733341 |
Snippet | Following the publication of an article by Soden, Hinton and Kaddour (Compos Sci Technol, V58, pp. 1225–54, 1998), which compared the predictions of 14... Following the publication of an article by Soden, Hinton and Kaddour (Compos Sci Technol, V58, pp. 1225-54, 1998), which compared the predictions of 14... |
SourceID | proquest crossref elsevier |
SourceType | Aggregation Database Publisher |
StartPage | 449 |
SubjectTerms | B. Stress–strain curves Failure criteria Multiaxial failure envelopes |
Title | A comparison of the predictive capabilities of current failure theories for composite laminates: additional contributions |
URI | https://dx.doi.org/10.1016/S0266-3538(03)00226-4 https://search.proquest.com/docview/28114784 |
Volume | 64 |
hasFullText | 1 |
inHoldings | 1 |
isFullTextHit | |
isPrint | |
link | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwnV07T8MwED71MQADggKiPIoHBhjSJrGTOGwVoiogukClbpadOFKXtOpjYOG3c3aSFpAQElMkO7Yi3_nuu_i7M8A1Q5CeJhxjEwS3Dktl6sg0Y44MooyGGh-2At_LKByO2dMkmNTgvsqFMbTK0vYXNt1a67KlV65mbz6d9l4xekBvSTmqqWvSQevQRHfk8wY0-4_Pw9HGIEeBvRvZvO-YAdtEnmIS23jj0ls7j8N-c1E_jLX1QIMD2C-hI-kXX3cINZ23YKfKLF62YO9LccEjeO-TZHPJIJllBKEemS_MwYwxcSRBN2mZsRgrm-6kqNREMjk1VHViUxxNH8JaO5Ohd2mCGjTNDUC9I4aLVPxKJJbxXl6dtTyG8eDh7X7olBctOAlz2cqJZRBkuPVpFJj4IVYhZ7FWTCkM_jyqQxkmiIyUVkr5QaKodJmMEVqFyg95RukJNPJZrk-BeLEOWOprj6cpi3ylpE-lTiSlfko9SdvQrdZWzIt6GmJLNENhCCMM4VJhhSFYG3glAfFNMQTa_L-GXlUSE7hpzEmIzPVsvRQ-xzAw4uzs_5Ofw25B4jF0tAtorBZrfYn4ZKU6UO9-eJ1SCz8B89Lhqg |
link.rule.ids | 315,783,787,4509,24128,27936,27937,45597,45691 |
linkProvider | Elsevier |
linkToHtml | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwnV07T8MwED6VMhQGxFOUVz0wwBCaxs6LrUJUBVoWWonNshNH6pJWfQws_HbunIQCEkJiimQ7VuQ7n7-Lv7sDuBQI0tMkQt8Ewa0jUpU6Ks2Eo_ww44HBh83AN3wO-mPx-Oq_1uCuioUhWmVp-wubbq112dIuV7M9m0zaL-g94GnJI1RTl8JBN2BTED5Gpb55X_M8Qt9WRqbRDg1fh_EUU9jGK5df21kc8dsB9cNU2_Ontws7JXBk3eLb9qBm8n1oVHHFi33Y_pJa8ADeuiz5LDHIphlDoMdmc7qWIQPHEjwkLS8WPWXqToo8TSxTEyKqMxvgSH0Iau1MRO4yDPVnkhM8vWXERCp-JDLLdy8LZy0OYdy7H931nbLMgpMIVyydWPl-hhufhz55D7EOIhEbLbRG16_DTaCCBHGRNlprz080V65QMQKrQHtBlHF-BPV8mptjYJ3Y-CL1TCdKUxF6WiuPK5Mozr2UdxRvwk21tnJWZNOQa5oZCkOSMKTLpRWGFE2IKgnIb2oh0eL_9WqrkpjELUP3ICo309VCehE6gWEkTv4_eQsa_dFwIAcPz0-nsFXQeYiYdgb15XxlzhGpLPWF1cQP-Tzigw |
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=A+comparison+of+the+predictive+capabilities+of+current+failure+theories+for+composite+laminates%3A+additional+contributions&rft.jtitle=Composites+science+and+technology&rft.au=Kaddour%2C+A+S&rft.au=Hinton%2C+M+J&rft.au=Soden%2C+P+D&rft.date=2004-03-01&rft.issn=0266-3538&rft.volume=64&rft.issue=3-4&rft.spage=449&rft.epage=476&rft_id=info:doi/10.1016%2FS0266-3538%2803%2900226-4&rft.externalDBID=NO_FULL_TEXT |
thumbnail_l | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=0266-3538&client=summon |
thumbnail_m | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=0266-3538&client=summon |
thumbnail_s | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=0266-3538&client=summon |