2021
DOI: 10.1002/mawe.202000119
|View full text |Cite
|
Sign up to set email alerts
|

Modal analysis of an aluminum beam coated with damaged and porous functionally graded material

Abstract: In this paper modal analysis is performed on a symmetric aluminum beam which is coated with functionally graded material containing porosities. A polynomial function is used to vary the density and elasticity through the thickness of the coating, while the effective elastic modulus and density are found with classical lamination theory. To achieve a truthful modeling the gradually changing mechanical properties of the coating are modeled as 25 layers of material, while each individual layer is isotropic and ho… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1
1
1

Citation Types

0
3
0

Year Published

2024
2024
2024
2024

Publication Types

Select...
1

Relationship

1
0

Authors

Journals

citations
Cited by 1 publication
(3 citation statements)
references
References 29 publications
0
3
0
Order By: Relevance
“…The stiffness and mass matrices of the original Timoshenko element are derived either with energy methods or by analytical derivation [32, 33]. However, in order for the model to allow for axial loads and deformations, the stiffness and mass matrix of a bar element is included to obtain the following stiffness and mass matrices of the modified Timoshenko beam element, as detailed in earlier research [21, 25]. The present approach can be summarized simply, Equations (7–: K=ρAa2313m1m2m3m4m2m5-m4m61323m3-m4m1-m2m4m6-m2m5+ρIz30a1+3β2m7m8-m7m8m8m9-m8m10-m7-m8m7-m8m8m10-m8m9 $\vcenter{\openup.5em\halign{$\displaystyle{#}$\cr \left[K\right]=\rho Aa\left[\begin{matrix}{{2}\over{3}} & & & {{1}\over{3}} & & \\ & {m}_{1} & {m}_{2} & & {m}_{3} & {m}_{4} \\ & {m}_{2} & {m}_{5} & & -{m}_{4} & {m}_{6} \\ {{1}\over{3}} & & & {{2}\over{3}} & & \\ & {m}_{3} & -{m}_{4} & & {m}_{1} & -{m}_{2} \\ & {m}_{4} & {m}_{6} & & -{m}_{2} & {m}_{5} \end{matrix} \right]+\hfill\cr {{\rho {I}_{z}}\over{30a{\left(1+3\beta \right)}^{2}}}\left[\begin{matrix} & & & ...…”
Section: Discussionmentioning
confidence: 99%
See 2 more Smart Citations
“…The stiffness and mass matrices of the original Timoshenko element are derived either with energy methods or by analytical derivation [32, 33]. However, in order for the model to allow for axial loads and deformations, the stiffness and mass matrix of a bar element is included to obtain the following stiffness and mass matrices of the modified Timoshenko beam element, as detailed in earlier research [21, 25]. The present approach can be summarized simply, Equations (7–: K=ρAa2313m1m2m3m4m2m5-m4m61323m3-m4m1-m2m4m6-m2m5+ρIz30a1+3β2m7m8-m7m8m8m9-m8m10-m7-m8m7-m8m8m10-m8m9 $\vcenter{\openup.5em\halign{$\displaystyle{#}$\cr \left[K\right]=\rho Aa\left[\begin{matrix}{{2}\over{3}} & & & {{1}\over{3}} & & \\ & {m}_{1} & {m}_{2} & & {m}_{3} & {m}_{4} \\ & {m}_{2} & {m}_{5} & & -{m}_{4} & {m}_{6} \\ {{1}\over{3}} & & & {{2}\over{3}} & & \\ & {m}_{3} & -{m}_{4} & & {m}_{1} & -{m}_{2} \\ & {m}_{4} & {m}_{6} & & -{m}_{2} & {m}_{5} \end{matrix} \right]+\hfill\cr {{\rho {I}_{z}}\over{30a{\left(1+3\beta \right)}^{2}}}\left[\begin{matrix} & & & ...…”
Section: Discussionmentioning
confidence: 99%
“…The stiffness and mass matrices of the original Timoshenko element are derived either with energy methods or by analytical derivation [32,33]. However, in order for the model to allow for axial loads and deformations, the stiffness and mass matrix of a bar element is included to obtain the following stiffness and mass matrices of the modified Timoshenko beam element, as detailed in earlier research [21,25]. The present approach can be summarized simply, Equations (7-10):…”
Section: Finite Element Modeling Of the Beammentioning
confidence: 99%
See 1 more Smart Citation