Investigation of exact analytical solutions for composite laminates under pin-bearing loading (Record no. 54485)

MARC details
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fixed length control field 02454nam a2200301Ia 4500
003 - CONTROL NUMBER IDENTIFIER
control field MX-MdCICY
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250625162448.0
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-20390
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fixed length control field 250602s9999 xx |||||s2 |||| ||und|d
245 10 - TITLE STATEMENT
Title Investigation of exact analytical solutions for composite laminates under pin-bearing loading
490 0# - SERIES STATEMENT
Volume/sequential designation Composite Structures, 292, p.115605, 2022
520 3# - SUMMARY, ETC.
Summary, etc. A number of analytical, experimental as well as numerical methods are available for designing mechanically fastened composite joints. In the present paper, exact analytical solutions previously introduced in literature for the case of a pin-loaded composite laminate are investigated. Experimental testing in a single-lap pin-bearing setup accompanied by digital image correlation of quasi-isotropic and highly-orthotropic CFRP laminates is conducted. Additionally, 3D finite element modeling is performed for detailed analysis of the test specimens on lamina level. Within a preliminary study, it is concluded that application of either of the analytical solutions leads to quantitative as well as qualitative differences in the resulting stress fields, thus, indicating that the choice of model is critical for subsequent failure analysis. Qualitative as well as quantitative comparisons of 2D strain fields on laminate level confirm the high prediction quality of certain analytical solutions. However, there are analytical solutions, some of which are implemented in commercial composite design software, that exhibit significant deviations from experimental and numerical data. These observations are further extended by detailed stress analysis down to lamina level. The results show that certain exact analytical solutions exhibit very good stress prediction qualities for w/d ratios as low as 3 and thus can be recommended for preliminary design purposes.
650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element LAMINATES
650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element STRESS CONCENTRATIONS
650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element ANALYTICAL MODELING
650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element FINITE ELEMENT ANALYSIS (FEA)
650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element LAMINATE MECHANICS
650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element MECHANICAL TESTING
650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element DIGITAL IMAGE CORRELATION (DIC)
700 12 - ADDED ENTRY--PERSONAL NAME
Personal name Koord, J.
700 12 - ADDED ENTRY--PERSONAL NAME
Personal name Stüven, J. L.
700 12 - ADDED ENTRY--PERSONAL NAME
Personal name Völkerink, O.
700 12 - ADDED ENTRY--PERSONAL NAME
Personal name Petersen, E.
700 12 - ADDED ENTRY--PERSONAL NAME
Personal name Hühne, C.
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier <a href="https://drive.google.com/file/d/1a8efrWPqQv0BSTlGQ67gTPhvSGbygeEI/view?usp=drivesdk">https://drive.google.com/file/d/1a8efrWPqQv0BSTlGQ67gTPhvSGbygeEI/view?usp=drivesdk</a>
Public note Para ver el documento ingresa a Google con tu cuenta: @cicy.edu.mx
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Source of classification or shelving scheme Clasificación local
Koha item type Documentos solicitados
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  Clasificación local     Ref1 CICY CICY Documento préstamo interbibliotecario 25.06.2025   B-20390 25.06.2025 25.06.2025 Documentos solicitados