Composite Structures Analysis by finite Element Method

Program taught in English.

 

Objectifs

The aim of this module is to provide an overview on Finite Element Structural Analysis for composite parts existing in an aircraft.

On completion of this module, delegates will be able to :

  • Understand Finite element sizing principles and tools for composite structures
  • Appreciate the dependency between these principles and the requirements and also aircraft design constraints
  • Describe and analyze FE simulation for individual system
  • Understand the influence of FE analysis on reliability, safety and economics of aircraft operation.

 

Public concerné

This module is intended for professionals - engineers or assistant engineers and/or managers- interested in a carrer on aeronautical maintenance engineering.

 

Pré-requis

Basis of theory of finite elements for isotropic materials and Classical Laminate Theory for Composite Materials.
On demand, a ten hour preparatory reading of reference litterature could be send to help the delegate to improve his knwoledge on this topics.

 

Programme

Theory of finite elements for composites :

  • Type of elements ; Meshing of composite structures
  • Post-processing / analysis of results

Practical use of composites finite element software :

  • Introduction
  • Analysis of finite element simulation on thin structures
  • Thick structures and Sandwich structures
  • Study of repaired structure
  • Buckling / post Buckling
  • Dynamics

Large displacement ; Non linear behavior
Industrial conferences

Frais d'inscription

1 250 € net inclusive of didactical material, coffee-breaks and lunches.

Modalités d'inscription

Number of delegates limited : 16 maximum

 

Durée : 5 jours

 

Prochaine session

 

Plaquette de présentation

 

Fiche d'inscription



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Dernière mise à jour : 21/12/2011

Responsable de cette page : Claire ROUX