Experimental and numerical investigation on the failure behavior of Bouligand laminates under off-axis open-hole tensile loading (Record no. 54938)

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control field MX-MdCICY
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250625162456.0
040 ## - CATALOGING SOURCE
Transcribing agency CICY
090 ## - LOCALLY ASSIGNED LC-TYPE CALL NUMBER (OCLC); LOCAL CALL NUMBER (RLIN)
Classification number (OCLC) (R) ; Classification number, CALL (RLIN) (NR) B-20858
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fixed length control field 250602s9999 xx |||||s2 |||| ||und|d
245 10 - TITLE STATEMENT
Title Experimental and numerical investigation on the failure behavior of Bouligand laminates under off-axis open-hole tensile loading
490 0# - SERIES STATEMENT
Volume/sequential designation Composite Structures, 313, p.116932, 2023
520 3# - SUMMARY, ETC.
Summary, etc. The Bouligand structure is a fibrous laminate with uniaxial layers assembled periodically into a helicoidal pattern. Compared to other types of laminates, its resistance to in-plane damage still lacks clarification. The failure behavior of Bouligand laminates under off-axis open-hole tensile (OHT)loading was investigated compared to cross-ply and quasi-isotropic structures using experiment and numerical simulation. After verifying the progressive damage model based on Hashin criteria, the numerical predictions from various off-axis loadings were compared between these three structures. The results show that Bouligand laminates exhibit low but nearly stable OHT strength. In comparison, the cross-ply structure exhibits high OHT strength variation when loaded in different directions. With the change of off-axis angle, the OHT strength of the Bouligand structure changes by 10.1 percent from 405.2 MPa to 364.1 MPa, while it changes by 69.1 percent from 533.8 MPa to 165.1 MPa for the cross-ply structure. Besides, the Bouligand structure exhibits higher OHT strength when the off-axis angle exceeds 5°. It also exhibits a more stable OHT strength than the quasi-isotropic structure. It is shown that the failure of fiber and matrix is the primary factor affecting the OHT strength of the laminate, while the delamination has little effect on the OHT strength.
650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element OPEN-HOLE LAMINATE
650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element BOULIGAND STRUCTURE
650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element OFF-AXIS TENSIÓN
650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element FAILURE MODE
700 12 - ADDED ENTRY--PERSONAL NAME
Personal name Luo, H.
700 12 - ADDED ENTRY--PERSONAL NAME
Personal name Wang, H.
700 12 - ADDED ENTRY--PERSONAL NAME
Personal name Zhao, Z.
700 12 - ADDED ENTRY--PERSONAL NAME
Personal name Xue, H.
700 12 - ADDED ENTRY--PERSONAL NAME
Personal name Li, Y.
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier <a href="https://drive.google.com/file/d/1UDJD1FeJ2BlBxW1JjFeJnYL_WFX8xmPC/view?usp=drivesdk">https://drive.google.com/file/d/1UDJD1FeJ2BlBxW1JjFeJnYL_WFX8xmPC/view?usp=drivesdk</a>
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Source of classification or shelving scheme Clasificación local
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  Clasificación local     Ref1 CICY CICY Documento préstamo interbibliotecario 25.06.2025   B-20858 25.06.2025 25.06.2025 Documentos solicitados