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Hygro-thermal buckling analysis of polymer–CNT–fiber-laminated nanocomposite disk under uniform lateral pressure with the aid of GDQM

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Abstract

In this research, we study the thermal buckling performance of multi-scale hybrid laminated nanocomposite (MHLC) disk (MHLCD) subjected hygro-mechanical loading. The matrix material is reinforced with carbon nanotubes (CNTs) or carbon fibers (CF) at the nano- or macro-scale, respectively. The disk is modeled based on higher order shear deformation theory. We present a modified Halpin–Tsai model to predict the effective properties of the MHLCD. The minimum total potential energy principle is employed to establish the governing equations of the system, which is finally solved by the generalized differential quadrature method. To validate the approach, numerical results are compared with available results from the literature. Subsequently, a comprehensive parameter study is carried out to quantify the influence of different parameters such as stiffness of the substrate, patterns of temperature increase, moisture coefficient, stacking sequence of the CFs, weight fraction and distribution patterns of CNTs, outer radius to inner radius ratio and inner radius to thickness ratio on the response of the plate. Some new results related to critical buckling of an MHLCD are also presented, which can serve as benchmark solutions for future investigations.

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Abbreviations

h, R i, and R o :

Thickness, the inner and outer radius of the disk, respectively

CNTs:

Carbon nanotubes

F and NCM:

Fiber and nanocomposite matrix, respectively

ρ, E, ν and G:

Density, Young’s module, Poisson’s ratio, and shear parameters, respectively

V NCM, V F :

Volume fractions of nanocomposite matrix and fiber, respectively

l CNT, t CNT, d CNT, E CNT and V CNT :

The length, thickness, diameter, Younge’s module, and volume fraction of carbon nanotubes, respectively

V *CNT , W CNT :

Effective volume fraction and weight fraction of the CNTs, respectively

N t, V CNT :

Layer number and volume fraction of CNTs, respectively

α 11 and α 22 :

Thermal expansion coefficients of the multi-scale hybrid nanocomposite

α NCM :

The thermal expansion coefficient of the nanocomposite matrix

\(\beta_{11} \,\,\,{\text{and}}\,\,\,\beta_{22}\) :

The moisture coefficients of the multi-scale hybrid laminated nanocomposite

β M :

The moisture coefficients of the matrix

U, V, W :

Displacement fields of a disk

u, v, w, ØR and Øθ :

The displacements of the mid-surface in R, θ and Z directions and rotations of the transverse normal around R and θ directions, respectively

ɛ RR and ɛ θθ :

The corresponding normal strains in R and θ directions, respectively

γ RZγ and γ θZ :

The shear strain in the RZ, Rθ and θZ plane

U*, W*:

Corresponding strain energy of the system, the work done, respectively

N T :

Applied forces due to variation of temperature

ΔT :

Temperature changes

N H :

Applied forces due to variation of hygro-loading

ΔH :

Moisture changes

K w and K p :

Winkler and Pasternak coefficients of the substrate

Q ij and \(\bar{Q}_{ij}\) :

Stiffness elements, stiffness elements relates to orientation angle and the orientation angle, respectively

θ :

The lamination angle with respect to the disk R-axis

N :

The number of distributed points along the R-axis

d, b, and δ :

d as a subscript stands for the domain grid points, b as subscript stands for boundary grid points and the displacement vector, respectively

F ij and K ij :

Components of force and stiffness matrices, respectively

\(F_{ij}^{*} \,{\text{and}}\,K_{ij}^{*}\) :

Components of force and stiffness matrices in the GDQ method, respectively

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Shandong University Science and Technology Project (J18KB163).

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Chen, H., Song, H., Li, Y. et al. Hygro-thermal buckling analysis of polymer–CNT–fiber-laminated nanocomposite disk under uniform lateral pressure with the aid of GDQM. Engineering with Computers 38, 1793–1817 (2022). https://doi.org/10.1007/s00366-020-01102-y

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