001471619 000__ 04110cam\\2200661\i\4500 001471619 001__ 1471619 001471619 003__ OCoLC 001471619 005__ 20230908003306.0 001471619 006__ m\\\\\o\\d\\\\\\\\ 001471619 007__ cr\cn\nnnunnun 001471619 008__ 230711s2023\\\\sz\a\\\\ob\\\\001\0\eng\d 001471619 019__ $$a1390117484 001471619 020__ $$a9783031329753$$q(electronic bk.) 001471619 020__ $$a3031329759$$q(electronic bk.) 001471619 020__ $$z9783031329746 001471619 020__ $$z3031329740 001471619 0247_ $$a10.1007/978-3-031-32975-3$$2doi 001471619 035__ $$aSP(OCoLC)1390096064 001471619 040__ $$aGW5XE$$beng$$erda$$epn$$cGW5XE$$dYDX$$dEBLCP$$dOCLCQ 001471619 049__ $$aISEA 001471619 050_4 $$aTA418.9.C6 001471619 08204 $$a620.1/180151$$223/eng/20230711 001471619 1001_ $$aÖchsner, Andreas,$$eauthor. 001471619 24512 $$aA numerical approach to the classical laminate theory of composite materials :$$bthe composite laminate analysis tool--CLAT v2.0 /$$cAndreas Öchsner, Resam Makvandi. 001471619 264_1 $$aCham :$$bSpringer,$$c[2023] 001471619 264_4 $$c©2023 001471619 300__ $$a1 online resource (xi, 170 pages) :$$billustrations. 001471619 336__ $$atext$$btxt$$2rdacontent 001471619 337__ $$acomputer$$bc$$2rdamedia 001471619 338__ $$aonline resource$$bcr$$2rdacarrier 001471619 4901_ $$aAdvanced structured materials,$$x1869-8441 ;$$vvolume 189 001471619 504__ $$aIncludes bibliographical references and index. 001471619 5050_ $$a1. Introduction -- 2. Classical Laminate Theory -- 3. Composite Laminate Analysis Tool - CLAT -- 4. Application Examples -- 5. Source Codes. 001471619 506__ $$aAccess limited to authorized users. 001471619 520__ $$aThis book first provides a systematic and thorough introduction to the classical laminate theory for composite materials based on the theory for plane elasticity elements and classical (shear-rigid) plate elements. The focus is on unidirectional lamina which can be described based on orthotropic constitutive equations and their composition to layered laminates. In addition to the elastic behavior, failure is investigated based on the maximum stress, maximum strain, Tsai-Hill, and the Tsai-Wu criteria. The solution of the fundamental equations of the classical laminate theory is connected with extensive matrix operations, and many problems require in addition iteration loops. Thus, a classical hand calculation of related problems is extremely time consuming. In order to facilitate the application of the classical laminate theory, we decided to provide a Python-based computational tool, the so-called Composite Laminate Analysis Tool (CLAT) to easily solve some standard questions from the context of fiber-reinforced composites. The tool runs in any standard web browser and offers a user-friendly interface with many post-processing options. The functionality comprises stress and strain analysis of lamina and laminates, derivation of off-axis elastic properties of lamina, and the failure analysis based on different criteria. 001471619 588__ $$aOnline resource; title from PDF title page (SpringerLink, viewed July 11, 2023). 001471619 650_0 $$aComposite materials$$xMathematics. 001471619 650_0 $$aComposite materials$$xData processing. 001471619 650_0 $$aLaminated materials$$xMathematics. 001471619 650_0 $$aLaminated materials$$xData processing. 001471619 655_0 $$aElectronic books. 001471619 7001_ $$aMakvandi, Resam,$$eauthor. 001471619 77608 $$iPrint version: $$z3031329740$$z9783031329746$$w(OCoLC)1375540591 001471619 830_0 $$aAdvanced structured materials ;$$v189.$$x1869-8441 001471619 852__ $$bebk 001471619 85640 $$3Springer Nature$$uhttps://univsouthin.idm.oclc.org/login?url=https://link.springer.com/10.1007/978-3-031-32975-3$$zOnline Access$$91397441.1 001471619 909CO $$ooai:library.usi.edu:1471619$$pGLOBAL_SET 001471619 980__ $$aBIB 001471619 980__ $$aEBOOK 001471619 982__ $$aEbook 001471619 983__ $$aOnline 001471619 994__ $$a92$$bISE