Bird impact resistance analysis of laminated glass structure

Sheng Zhi Tan; Xiao Hu Yao; Peng Yu; Long Hui Zhang; Shu Guang Zang

doi:10.15918/j.tbit1001-0645.2016.Suppl.1.042

Bird impact resistance analysis of laminated glass structure

Sheng Zhi Tan, Xiao Hu Yao^*, Peng Yu, Long Hui Zhang, Shu Guang Zang

^*Corresponding author for this work

Research output: Contribution to journal › Article › peer-review

2 Citations (Scopus)

Abstract

Bird impact resistant design is a complex and key procedure in aircraft design. The coupling of smoothed particle hydrodynamics (SPH) with finite element method (FEM) was presented to model bird impacting on the laminated glass structure consisting of inorganic glass, polyurethane (PU), polycarbonate (PC) andpolymethyl methacrylate (PMMA). Material properties of the transparent material mentioned above were obtained by quasi-static and dynamic experiment result, respectively. The dynamic response of laminated glass structure with bird impact was obtained by simulations using the commercial software LS-DYNA. The damage and failure processes of laminated glass structure were observed and the bird impact resistance of laminated glass structure was analyzed. It is found that the structure consisting of inorganic glass and polymer has the best bird impact resistant performance.

Original language	English
Pages (from-to)	170-173
Number of pages	4
Journal	Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology
Volume	36
DOIs	https://doi.org/10.15918/j.tbit1001-0645.2016.Suppl.1.042
Publication status	Published - 1 Jun 2016
Externally published	Yes

Keywords

Bird impact
Damage and failure
Laminated glass structure
Numerical calculation

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10.15918/j.tbit1001-0645.2016.Suppl.1.042

Cite this

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title = "Bird impact resistance analysis of laminated glass structure",

abstract = "Bird impact resistant design is a complex and key procedure in aircraft design. The coupling of smoothed particle hydrodynamics (SPH) with finite element method (FEM) was presented to model bird impacting on the laminated glass structure consisting of inorganic glass, polyurethane (PU), polycarbonate (PC) andpolymethyl methacrylate (PMMA). Material properties of the transparent material mentioned above were obtained by quasi-static and dynamic experiment result, respectively. The dynamic response of laminated glass structure with bird impact was obtained by simulations using the commercial software LS-DYNA. The damage and failure processes of laminated glass structure were observed and the bird impact resistance of laminated glass structure was analyzed. It is found that the structure consisting of inorganic glass and polymer has the best bird impact resistant performance.",

keywords = "Bird impact, Damage and failure, Laminated glass structure, Numerical calculation",

author = "Tan, {Sheng Zhi} and Yao, {Xiao Hu} and Peng Yu and Zhang, {Long Hui} and Zang, {Shu Guang}",

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doi = "10.15918/j.tbit1001-0645.2016.Suppl.1.042",

language = "English",

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T1 - Bird impact resistance analysis of laminated glass structure

AU - Tan, Sheng Zhi

AU - Yao, Xiao Hu

AU - Yu, Peng

AU - Zhang, Long Hui

AU - Zang, Shu Guang

PY - 2016/6/1

Y1 - 2016/6/1

N2 - Bird impact resistant design is a complex and key procedure in aircraft design. The coupling of smoothed particle hydrodynamics (SPH) with finite element method (FEM) was presented to model bird impacting on the laminated glass structure consisting of inorganic glass, polyurethane (PU), polycarbonate (PC) andpolymethyl methacrylate (PMMA). Material properties of the transparent material mentioned above were obtained by quasi-static and dynamic experiment result, respectively. The dynamic response of laminated glass structure with bird impact was obtained by simulations using the commercial software LS-DYNA. The damage and failure processes of laminated glass structure were observed and the bird impact resistance of laminated glass structure was analyzed. It is found that the structure consisting of inorganic glass and polymer has the best bird impact resistant performance.

AB - Bird impact resistant design is a complex and key procedure in aircraft design. The coupling of smoothed particle hydrodynamics (SPH) with finite element method (FEM) was presented to model bird impacting on the laminated glass structure consisting of inorganic glass, polyurethane (PU), polycarbonate (PC) andpolymethyl methacrylate (PMMA). Material properties of the transparent material mentioned above were obtained by quasi-static and dynamic experiment result, respectively. The dynamic response of laminated glass structure with bird impact was obtained by simulations using the commercial software LS-DYNA. The damage and failure processes of laminated glass structure were observed and the bird impact resistance of laminated glass structure was analyzed. It is found that the structure consisting of inorganic glass and polymer has the best bird impact resistant performance.

KW - Bird impact

KW - Damage and failure

KW - Laminated glass structure

KW - Numerical calculation

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U2 - 10.15918/j.tbit1001-0645.2016.Suppl.1.042

DO - 10.15918/j.tbit1001-0645.2016.Suppl.1.042

M3 - Article

AN - SCOPUS:84992206000

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JO - Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology

JF - Beijing Ligong Daxue Xuebao/Transaction of Beijing Institute of Technology

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Bird impact resistance analysis of laminated glass structure

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Keywords

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