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 in | Composite structures Vol. 94; no. 1; pp. 15 - 23 |
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Main Authors | , |
Format | Journal Article |
Language | English |
Published |
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01.12.2011
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ISSN | 0263-8223 1879-1085 |
DOI | 10.1016/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. |
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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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Cites_doi | 10.1016/j.compstruct.2009.12.006 10.1016/S0266-3538(03)00227-6 10.1016/S0266-3538(01)00202-0 10.1016/j.ijimpeng.2009.03.009 10.1016/S0263-8223(03)00033-3 10.1016/j.cma.2003.12.061 10.1016/j.compositesa.2006.02.018 10.1016/S0263-8223(02)00050-8 10.1016/j.compscitech.2010.12.024 10.1007/s10443-008-9070-6 10.1016/S0266-3538(96)00140-6 10.1023/B:ACMA.0000037133.64496.13 10.1016/j.ijimpeng.2004.09.004 10.1023/B:ACMA.0000037134.93410.c0 10.1016/j.ijimpeng.2005.04.011 10.1016/0010-4361(89)90913-0 |
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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 |
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model publication-title: Appl Compos Mater doi: 10.1023/B:ACMA.0000037134.93410.c0 – ident: 10.1016/j.compstruct.2011.07.028_b0030 – volume: 32 start-page: 1651 year: 2006 ident: 10.1016/j.compstruct.2011.07.028_b0035 article-title: Modelling of impact forces and pressures in lagrangian bird strike analyses publication-title: Int J Imp Eng doi: 10.1016/j.ijimpeng.2005.04.011 – volume: 20 start-page: 545 year: 1989 ident: 10.1016/j.compstruct.2011.07.028_b0090 article-title: Comparison of the low and high velocity impact response CFRP publication-title: Composites doi: 10.1016/0010-4361(89)90913-0 |
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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 |
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