Johnson, Alastair and Holzapfel, Martin (2006) Numerical prediction of damage in composite structures from soft body impact. Journal of Materials Science, 41 (20).
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The paper summarises recent progress on materials modelling and numerical simulation of soft body impact damage in fibre reinforced composite aircraft structures. The work is based on the application of finite element (FE) analysis codes to simulate damage in composite shell structures under impact loads. Composites ply damage models and interply delamination models have been developed and implemented in commercial explicit FE codes. Models are discussed for predicting impact loads on aircraft structures arising from deformable soft bodies such as gelatine (synthetic bird) and ice (hailstone). The composites failure models and code developments are briefly summarised and applied in the paper to numerical simulation of synthetic bird impact on idealised composite aircraft structures.
|Title:||Numerical prediction of damage in composite structures from soft body impact|
|Journal or Publication Title:||Journal of Materials Science|
|In ISI Web of Science:||Yes|
|Keywords:||composite structures, damage mechanics, impact simulation, soft body impact|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Aircraft Research|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L AR - Aircraft Research|
|DLR - Research theme (Project):||L - Structures & Materials|
|Institutes and Institutions:||Institute of Structures and Design > Structural Integrity|
|Deposited By:||Dr.phil. Alastair Johnson|
|Deposited On:||28 Dec 2006|
|Last Modified:||27 Apr 2009 13:17|
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