Impact of aircraft rubber tyre fragments on aluminium alloy plates: II—Numerical simulation using LS-DYNA

A discrete model for a reinforced rubber-like material is proposed in order to simulate numerically a debris tyre impact on a typical structure of an aircraft when using the FE code LS-DYNA. The model is calibrated using the static and dynamic test data for the actual tyre material. The dynamics of...

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Published inInternational journal of impact engineering Vol. 34; no. 4; pp. 647 - 667
Main Authors Karagiozova, D., Mines, R.A.W.
Format Journal Article
LanguageEnglish
Published Oxford Elsevier Ltd 01.04.2007
Elsevier Science
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Online AccessGet full text
ISSN0734-743X
1879-3509
DOI10.1016/j.ijimpeng.2006.02.004

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Abstract A discrete model for a reinforced rubber-like material is proposed in order to simulate numerically a debris tyre impact on a typical structure of an aircraft when using the FE code LS-DYNA. The model is calibrated using the static and dynamic test data for the actual tyre material. The dynamics of the tyre projectile is validated when comparing the numerical predictions with the response of a square aluminium alloy plate subject to a ribbon projectile impact having different initial velocities and impacting the plate at an angle of 30°. Good agreement is obtained in terms of the strains in the plate caused by the ribbon impact. The numerically predicted deformations of the projectile also represent well the dynamics of the tyre ribbon recorded during the experiments. Some characteristic features of a soft projectile impact on a deformable plate are discussed. The developed model is then extended to the simulation of a full-scale impact test, and good agreement is shown between experiment and simulation.
AbstractList A discrete model for a reinforced rubber-like material is proposed in order to simulate numerically a debris tyre impact on a typical structure of an aircraft when using the FE code LS-DYNA. The model is calibrated using the static and dynamic test data for the actual tyre material. The dynamics of the tyre projectile is validated when comparing the numerical predictions with the response of a square aluminium alloy plate subject to a ribbon projectile impact having different initial velocities and impacting the plate at an angle of 30 deg . Good agreement is obtained in terms of the strains in the plate caused by the ribbon impact. The numerically predicted deformations of the projectile also represent well the dynamics of the tyre ribbon recorded during the experiments. Some characteristic features of a soft projectile impact on a deformable plate are discussed. The developed model is then extended to the simulation of a full-scale impact test, and good agreement is shown between experiment and simulation.
A discrete model for a reinforced rubber-like material is proposed in order to simulate numerically a debris tyre impact on a typical structure of an aircraft when using the FE code LS-DYNA. The model is calibrated using the static and dynamic test data for the actual tyre material. The dynamics of the tyre projectile is validated when comparing the numerical predictions with the response of a square aluminium alloy plate subject to a ribbon projectile impact having different initial velocities and impacting the plate at an angle of 30°. Good agreement is obtained in terms of the strains in the plate caused by the ribbon impact. The numerically predicted deformations of the projectile also represent well the dynamics of the tyre ribbon recorded during the experiments. Some characteristic features of a soft projectile impact on a deformable plate are discussed. The developed model is then extended to the simulation of a full-scale impact test, and good agreement is shown between experiment and simulation.
Author Karagiozova, D.
Mines, R.A.W.
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  givenname: R.A.W.
  surname: Mines
  fullname: Mines, R.A.W.
  email: R.Mines@liverpool.ac.uk
  organization: Impact Research Centre, University of Liverpool, Brownlow Street, Liverpool, L69 3GH, England
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Cites_doi 10.1002/(SICI)1099-0887(199612)12:12<897::AID-CNM981>3.0.CO;2-D
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Issue 4
Keywords Reinforced rubber
Numerical simulation
Discrete material model
Soft impact
Aluminium alloy
Experimental study
Particle collision
Modeling
Deformable body
Dynamic test
Finite element method
Tyre
Rectangular plate
Rubber
Aircraft
Impact test
Static test
Mechanical shock
Language English
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Snippet A discrete model for a reinforced rubber-like material is proposed in order to simulate numerically a debris tyre impact on a typical structure of an aircraft...
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SubjectTerms Applied sciences
Discrete material model
Elastomers
Exact sciences and technology
Fracture mechanics (crack, fatigue, damage...)
Fundamental areas of phenomenology (including applications)
Industrial polymers. Preparations
Numerical simulation
Physics
Polymer industry, paints, wood
Reinforced rubber
Soft impact
Solid mechanics
Structural and continuum mechanics
Technology of polymers
Title Impact of aircraft rubber tyre fragments on aluminium alloy plates: II—Numerical simulation using LS-DYNA
URI https://dx.doi.org/10.1016/j.ijimpeng.2006.02.004
https://www.proquest.com/docview/29363284
Volume 34
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