Low-velocity heavy-mass impact response of slender metal foam core sandwich beam

The objective of this work is to investigate the dynamic large deflection response of fully clamped metal foam core sandwich beam struck by a low-velocity heavy mass. Analytical solution and ‘bounds’ of dynamic solutions are derived, respectively. Also, finite element analysis is carried out to obta...

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Published inComposite structures Vol. 93; no. 6; pp. 1526 - 1537
Main Authors Qin, Qing Hua, Wang, T.J.
Format Journal Article
LanguageEnglish
Published Kidlington Elsevier Ltd 01.05.2011
Elsevier
Subjects
Online AccessGet full text
ISSN0263-8223
1879-1085
DOI10.1016/j.compstruct.2010.11.018

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Abstract The objective of this work is to investigate the dynamic large deflection response of fully clamped metal foam core sandwich beam struck by a low-velocity heavy mass. Analytical solution and ‘bounds’ of dynamic solutions are derived, respectively. Also, finite element analysis is carried out to obtain the numerical solution of the problem. Comparisons of the dynamic, the quasi-static and numerical solutions for the non-dimensional maximum deflection of the sandwich beam with non-dimensional initial kinetic energy of the striker are presented for different cases of mass ratio, impact velocity and location. It is seen that the dynamic solution approaches the quasi-static one as the mass ratio of the striker to the beam is large enough, the quasi-static solution is in good agreement with the numerical results and both solutions lie in the ‘bounds’ of dynamic solutions. The quasi-static and numerical results for the impact force against the maximum deflection of the sandwich beam are obtained. It shows that the quasi-static solution can offer adequate accuracy to predict the low-velocity heavy-mass impact response of fully clamped sandwich beam.
AbstractList The objective of this work is to investigate the dynamic large deflection response of fully clamped metal foam core sandwich beam struck by a low-velocity heavy mass. Analytical solution and ‘bounds’ of dynamic solutions are derived, respectively. Also, finite element analysis is carried out to obtain the numerical solution of the problem. Comparisons of the dynamic, the quasi-static and numerical solutions for the non-dimensional maximum deflection of the sandwich beam with non-dimensional initial kinetic energy of the striker are presented for different cases of mass ratio, impact velocity and location. It is seen that the dynamic solution approaches the quasi-static one as the mass ratio of the striker to the beam is large enough, the quasi-static solution is in good agreement with the numerical results and both solutions lie in the ‘bounds’ of dynamic solutions. The quasi-static and numerical results for the impact force against the maximum deflection of the sandwich beam are obtained. It shows that the quasi-static solution can offer adequate accuracy to predict the low-velocity heavy-mass impact response of fully clamped sandwich beam.
Author Wang, T.J.
Qin, Qing Hua
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Issue 6
Keywords Sandwich beam
Overall bending
Low-velocity impact
Metal foam core
High strain
Vibration
Low speed
Sandwich structure
Quasi static theory
Porous material
Modeling
Finite element method
Metal foam
Kinetic energy
Mechanical shock
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Snippet The objective of this work is to investigate the dynamic large deflection response of fully clamped metal foam core sandwich beam struck by a low-velocity...
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SubjectTerms Beams (structural)
Clamping
Deflection
Dynamic tests
Dynamics
Exact sciences and technology
Fundamental areas of phenomenology (including applications)
Impact response
Low-velocity impact
Mathematical analysis
Mathematical models
Metal foam core
Overall bending
Physics
Sandwich beam
Solid mechanics
Static elasticity (thermoelasticity...)
Structural and continuum mechanics
Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)
Title Low-velocity heavy-mass impact response of slender metal foam core sandwich beam
URI https://dx.doi.org/10.1016/j.compstruct.2010.11.018
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https://www.proquest.com/docview/864395159
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