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020 _a9783031479847
_9978-3-031-47984-7
024 7 _a10.1007/978-3-031-47984-7
_2doi
050 4 _aQA808.2
072 7 _aPHD
_2bicssc
072 7 _aSCI065000
_2bisacsh
072 7 _aPHD
_2thema
100 1 _aÖchsner, Andreas.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_968776
245 1 2 _aA Numerical Approach to the Simplified Laminate Theory of Composite Materials
_h[electronic resource] :
_bThe Composite Laminate Analysis Tool—CLAT 1D /
_cby Andreas Öchsner, Resam Makvandi.
250 _a1st ed. 2024.
264 1 _aCham :
_bSpringer Nature Switzerland :
_bImprint: Springer,
_c2024.
300 _aXII, 146 p. 104 illus., 49 illus. in color.
_bonline resource.
336 _atext
_btxt
_2rdacontent
337 _acomputer
_bc
_2rdamedia
338 _aonline resource
_bcr
_2rdacarrier
347 _atext file
_bPDF
_2rda
490 1 _aAdvanced Structured Materials,
_x1869-8441 ;
_v202
505 0 _aIntroduction -- Simplified Laminate Theory -- Composite Laminate Analysis Tool – CLAT 1D -- Application Examples -- Source Codes -- Index.
520 _aA typical approach to treat composite materials, which are composed of layered unidirectional lamina, is the so-called classical laminate theory (CLT). This theory is based on the theory for plane elasticity elements and classical (shear-rigid) plate elements under the assumption of orthotropic constitutive equations. The solution of the fundamental equations of the classical laminate theory is connected with extensive matrix operations and many problems require in addition iteration loops. This two-dimensional approach and the underlying advanced continuum mechanical modeling might be very challenging for some students, particularly at universities of applied sciences. Thus, a reduced approach, the so-called simplified classical laminate theory (SCLT), has been recently proposed. The idea was to use solely isotropic one-dimensional elements, i.e., a superposition of bar and beam elements, to introduce the major calculation steps of the classical laminate theory. Understanding this simplified theory is much easier and the final step it to highlight the differences when moving to the general two-dimensional case. This monograph first provides a systematic and thorough introduction to the simplified laminate theory based on the theory for bars and classical beam plate elements. The focus is on stacking of isotropic layers to simplified laminates. In addition to the elastic behavior, failure is investigated based on the maximum stress, maximum strain, Tsai-Hill, and the Tsai-Wu criteria. We provide a Python-based computational tool, the so-called Composite Laminate Analysis Tool (CLAT 1D) to easily solve some standard questions from the context of fiber reinforced composites. The tool runs in any standard web browser and offers a user-friendly interface with many post-processing options. The functionality comprises stress and strain analysis of simplified lamina and laminates and the failure analysis based on different criteria.
650 0 _aContinuum mechanics.
650 0 _aComposite materials.
650 0 _aMathematics
_xData processing.
_965715
650 1 4 _aContinuum Mechanics.
650 2 4 _aComposites.
650 2 4 _aComputational Mathematics and Numerical Analysis.
_966073
700 1 _aMakvandi, Resam.
_eauthor.
_4aut
_4http://id.loc.gov/vocabulary/relators/aut
_970875
710 2 _aSpringerLink (Online service)
773 0 _tSpringer Nature eBook
776 0 8 _iPrinted edition:
_z9783031479830
776 0 8 _iPrinted edition:
_z9783031479854
776 0 8 _iPrinted edition:
_z9783031479861
830 0 _aAdvanced Structured Materials,
_x1869-8441 ;
_v202
_968737
856 4 0 _uhttps://doi.org/10.1007/978-3-031-47984-7
912 _aZDB-2-SMA
912 _aZDB-2-SXMS
999 _c57577
_d57577