東華大學圖書館 |

語系: 繁體中文

說明(常見問題)

回圖書館首頁

手機版館藏查詢

登入

回首頁

切換: 標籤 | MARC模式 | ISBD

FindBook

Google Book

Amazon

博客來

A numerical approach to the simplified laminate theory of composite materials = The Composite Laminate Analysis Tool -- CLAT 1D /

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	A numerical approach to the simplified laminate theory of composite materials/ by Andreas Ochsner, Resam Makvandi.
其他題名:	The Composite Laminate Analysis Tool -- CLAT 1D /
作者:	Ochsner, Andreas.
other author:	Makvandi, Resam.
Published:	Cham :Springer Nature Switzerland : : 2024.,
Description:	xii, 146 p. :ill. (some col.), digital ;24 cm.
[NT 15003449]:	Introduction -- Simplified Laminate Theory -- Composite Laminate Analysis Tool - CLAT 1D -- Application Examples -- Source Codes -- Index.
Contained By:	Springer Nature eBook
Subject:	Composite materials. -
Online resource:	https://doi.org/10.1007/978-3-031-47984-7
ISBN:	9783031479847

A numerical approach to the simplified laminate theory of composite materials = The Composite Laminate Analysis Tool -- CLAT 1D /
Ochsner, Andreas.

A numerical approach to the simplified laminate theory of composite materialsThe Composite Laminate Analysis Tool -- CLAT 1D /[electronic resource] :by Andreas Ochsner, Resam Makvandi. - Cham :Springer Nature Switzerland :2024. - xii, 146 p. :ill. (some col.), digital ;24 cm. - Advanced structured materials,v. 2021869-8441 ;. - Advanced structured materials ;v. 202..

Introduction -- Simplified Laminate Theory -- Composite Laminate Analysis Tool - CLAT 1D -- Application Examples -- Source Codes -- Index.

A 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.

ISBN: 9783031479847

Standard No.: 10.1007/978-3-031-47984-7doiSubjects--Topical Terms:

654082
Composite materials.

LC Class. No.: TA418.9.C6

Dewey Class. No.: 620.118

A numerical approach to the simplified laminate theory of composite materials = The Composite Laminate Analysis Tool -- CLAT 1D /
LDR:03244nmm a2200337 a 4500 001 2369223
003 DE-He213
005 20240212013926.0
006 m d
007 cr nn 008maaau
008 241127s2024 sz s 0 eng d
020 $a 9783031479847 $q (electronic bk.)
020 $a 9783031479830 $q (paper)
024 7 $a 10.1007/978-3-031-47984-7 $2 doi
035 $a 978-3-031-47984-7
040 $a GP $c GP
041 0 $a eng
050 4 $a TA418.9.C6
072 7 $a PHD $2 bicssc
072 7 $a SCI041000 $2 bisacsh
072 7 $a PHD $2 thema
082 0 4 $a 620.118 $2 23
090 $a TA418.9.C6 $b O16 2024
100 1 $a Ochsner, Andreas. $3 924194
245 1 2 $a A numerical approach to the simplified laminate theory of composite materials $h [electronic resource] : $b The Composite Laminate Analysis Tool -- CLAT 1D / $c by Andreas Ochsner, Resam Makvandi.
260 $a Cham : $b Springer Nature Switzerland : $b Imprint: Springer, $c 2024.
300 $a xii, 146 p. : $b ill. (some col.), digital ; $c 24 cm.
490 1 $a Advanced structured materials, $x 1869-8441 ; $v v. 202
505 0 $a Introduction -- Simplified Laminate Theory -- Composite Laminate Analysis Tool - CLAT 1D -- Application Examples -- Source Codes -- Index.
520 $a A 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 $a Composite materials. $3 654082
650 1 4 $a Continuum Mechanics. $3 3538810
650 2 4 $a Composites. $3 794662
650 2 4 $a Computational Mathematics and Numerical Analysis. $3 891040
700 1 $a Makvandi, Resam. $3 3378870
710 2 $a SpringerLink (Online service) $3 836513
773 0 $t Springer Nature eBook
830 0 $a Advanced structured materials ; $v v. 202. $3 3713733
856 4 0 $u https://doi.org/10.1007/978-3-031-47984-7
950 $a Mathematics and Statistics (SpringerNature-11649)