Progressive failure analysis for aeronautic composite structures / Najlacnejšie knihy
Progressive failure analysis for aeronautic composite structures

Kód: 16091025

Progressive failure analysis for aeronautic composite structures

Autor Marcelo Ribeiro, Volnei Tita

Recent improvements in manufacturing processes and materials properties associated with excellent mechanical characteristics and low weight have became composite materials very attractive for application on civil aircraft structur ... celý popis

62.24

Bežne: 72.96 €

Ušetríte 10.72 €


Skladom u dodávateľa
Odosielame za 5 - 8 dní
Pridať medzi želanie

Mohlo by sa vám tiež páčiť

Darujte túto knihu ešte dnes
  1. Objednajte knihu a vyberte Zaslať ako darček.
  2. Obratom obdržíte darovací poukaz na knihu, ktorý môžete ihneď odovzdať obdarovanému.
  3. Knihu zašleme na adresu obdarovaného, o nič sa nestaráte.

Viac informácií

Viac informácií o knihe Progressive failure analysis for aeronautic composite structures

Nákupom získate 151 bodov

Anotácia knihy

Recent improvements in manufacturing processes and materials properties associated with excellent mechanical characteristics and low weight have became composite materials very attractive for application on civil aircraft structures. However, even new designs are still very conservative, because the composite structure failure phenomena are very complex. Several failure criteria and theories have been developed to describe the damage process and how it evolves, but the solution of the problem is still open. Moreover, modern manufacturing processes, e.g. filament winding, have been used to produce a wide variety of structural shapes. Therefore, this work presents the development of a damage model and its application to simulate the progressive failure of flat composite laminates as well as for composite cylinders made by filament winding process. The proposed damage model has been implemented as a UMAT (User Material Subroutine) and VUMAT (User Material Subroutine for explicit simulations), which were linked to ABAQUSTM Finite Element (FE) commercial package. Progressive failure analyses have been carried out using FE Method in order to simulate the failure of filament wound.

Parametre knihy

62.24

Obľúbené z iného súdka



Osobný odber Bratislava a 12820 dalších

Copyright ©2008-26 najlacnejsie-knihy.sk Všetky práva vyhradenéSúkromieCookies


Môj účet: Prihlásiť sa
Všetky knihy sveta na jednom mieste. Navyše za skvelé ceny.

Nákupný košík ( prázdny )

Vyzdvihnutie v Zásielkovni
zadarmo nad 59,99 €.

Nachádzate sa: