Hybrid approach in bird strike damage prediction on aeronautical composite structures

► Coupled Eulerian Lagrangian formulation is used to simulate bird strike damage. ► LESAD program is developed as to automatically create input files for simulation. ► Hydrodynamic material models are programmed replicating bird loading during impact. ► Puck’s and Hashin’s failure criteria for compo...

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Published inComposite structures Vol. 94; no. 1; pp. 15 - 23
Main Authors Ivančević, D., Smojver, I.
Format Journal Article
LanguageEnglish
Published Kidlington Elsevier Ltd 01.12.2011
Elsevier
Subjects
Online AccessGet full text
ISSN0263-8223
1879-1085
DOI10.1016/j.compstruct.2011.07.028

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Abstract ► Coupled Eulerian Lagrangian formulation is used to simulate bird strike damage. ► LESAD program is developed as to automatically create input files for simulation. ► Hydrodynamic material models are programmed replicating bird loading during impact. ► Puck’s and Hashin’s failure criteria for composites are compared and validated. ► The damage prediction procedure is applied on a complex aeronautical structure. This paper deals with the problem of numerical prediction of bird strike induced damage on aeronautical structures. The problem of soft body impacts has been tackled by applying a hybrid Eulerian Lagrangian technique, thereby avoiding numerical difficulties associated with extensive mesh distortion. Eulerian modeling of the bird impactor resulted in a more realistic behavior of bird material during impact, which has lead to an enhanced response of the impacted structure. The work presented in this paper is focused on damage modeling in composite items of aeronautical structures. The bird impactor model and damage modeling approaches have been validated by comparison with experimental gas gun results available in the open literature, while the complete damage prediction procedure has been demonstrated on a complex airplane flap structure finite element model.
AbstractList This paper deals with the problem of numerical prediction of bird strike induced damage on aeronautical structures. The problem of soft body impacts has been tackled by applying a hybrid Eulerian Lagrangian technique, thereby avoiding numerical difficulties associated with extensive mesh distortion. Eulerian modeling of the bird impactor resulted in a more realistic behavior of bird material during impact, which has lead to an enhanced response of the impacted structure. The work presented in this paper is focused on damage modeling in composite items of aeronautical structures. The bird impactor model and damage modeling approaches have been validated by comparison with experimental gas gun results available in the open literature, while the complete damage prediction procedure has been demonstrated on a complex airplane flap structure finite element model.
► Coupled Eulerian Lagrangian formulation is used to simulate bird strike damage. ► LESAD program is developed as to automatically create input files for simulation. ► Hydrodynamic material models are programmed replicating bird loading during impact. ► Puck’s and Hashin’s failure criteria for composites are compared and validated. ► The damage prediction procedure is applied on a complex aeronautical structure. This paper deals with the problem of numerical prediction of bird strike induced damage on aeronautical structures. The problem of soft body impacts has been tackled by applying a hybrid Eulerian Lagrangian technique, thereby avoiding numerical difficulties associated with extensive mesh distortion. Eulerian modeling of the bird impactor resulted in a more realistic behavior of bird material during impact, which has lead to an enhanced response of the impacted structure. The work presented in this paper is focused on damage modeling in composite items of aeronautical structures. The bird impactor model and damage modeling approaches have been validated by comparison with experimental gas gun results available in the open literature, while the complete damage prediction procedure has been demonstrated on a complex airplane flap structure finite element model.
Author Smojver, I.
Ivančević, D.
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Issue 1
Keywords Bird strike
Composite structures
Aeronautical structures
Impact damage
Euler Lagrange equation
Control surface
Experimental study
Modeling
Finite element method
Vertebrata
Flap
Deflector
Aves
Gas gun
Aircraft
Impact test
Mesh generation
Trailing edge
Mechanical shock
Damaging
Language English
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Snippet ► Coupled Eulerian Lagrangian formulation is used to simulate bird strike damage. ► LESAD program is developed as to automatically create input files for...
This paper deals with the problem of numerical prediction of bird strike induced damage on aeronautical structures. The problem of soft body impacts has been...
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SubjectTerms Aeronautical structures
Aeronautics
Bird impact
Bird strike
Composite structures
Damage
Distortion
Exact sciences and technology
Finite element method
Fracture mechanics (crack, fatigue, damage...)
Fundamental areas of phenomenology (including applications)
Impact damage
Impactors
Mathematical models
Measurement and testing methods
Physics
Solid mechanics
Structural and continuum mechanics
Title Hybrid approach in bird strike damage prediction on aeronautical composite structures
URI https://dx.doi.org/10.1016/j.compstruct.2011.07.028
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