A Numerical Approach to the Simplified Laminate Theory of Composite Materials
The Composite Laminate Analysis Tool—CLAT 1D
Series: Advanced Structured Materials; 202;
- Publisher's listprice EUR 139.09
-
57 687 Ft (54 940 Ft + 5% VAT)
The price is estimated because at the time of ordering we do not know what conversion rates will apply to HUF / product currency when the book arrives. In case HUF is weaker, the price increases slightly, in case HUF is stronger, the price goes lower slightly.
- Discount 20% (cc. 11 537 Ft off)
- Discounted price 46 150 Ft (43 952 Ft + 5% VAT)
Subcribe now and take benefit of a favourable price.
Subscribe
57 687 Ft
Availability
printed on demand
Why don't you give exact delivery time?
Delivery time is estimated on our previous experiences. We give estimations only, because we order from outside Hungary, and the delivery time mainly depends on how quickly the publisher supplies the book. Faster or slower deliveries both happen, but we do our best to supply as quickly as possible.
Product details:
- Edition number 1st ed. 2024
- Publisher Springer Nature Switzerland
- Date of Publication 12 February 2024
- Number of Volumes 1 pieces, Book
- ISBN 9783031479830
- Binding Hardback
- No. of pages146 pages
- Size 235x155 mm
- Weight 442 g
- Language English
- Illustrations XII, 146 p. 104 illus., 49 illus. in color. Illustrations, black & white 528
Categories
Long description:
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. Understandingthis 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.
Table of Contents:
Introduction.- Simplified Laminate Theory.- Composite Laminate Analysis Tool – CLAT 1D.- Application Examples.- Source Codes.- Index.
More
