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Damage Tolerance of Aeronautical Sandwich Structures

  • D. Guedra-Degeorges
  • P. Thevenet
  • S. Maison
Conference paper

Abstract

The aim of this paper is to give an overview of the present aeronautical applications of sandwich materials and to describe the present damage tolerance approaches versus type of defects like debonding or impact. Some research orientations are proposed in order to improve, on the one hand, experimental identification of defect behaviour and, on the other hand, numerical simulation of aeronautical sandwich structures including such defects.

Keywords

Impact Energy Sandwich Structure Damage Tolerance Sandwich Specimen Stiffness Design 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer Science+Business Media Dordrecht 1998

Authors and Affiliations

  • D. Guedra-Degeorges
    • 1
  • P. Thevenet
    • 1
  • S. Maison
    • 1
  1. 1.Aérospatiale — Centre Commun de Recherches Louis BlériotSuresnesFrance

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