A comprehensive investigation on nonlinear vibration andbending characteristics of bio-inspired helicoidallaminated composite structures

doi:10.1007/s10483-025-3200-7

摘要/Abstract

Abstract:

Bio-inspired helicoidal composite laminates, inspired by the intricate helical structures found in nature, present a promising frontier for enhancing the mechanical properties of structural designs. Hence, this study provides a comprehensive investigation into the nonlinear free vibration and nonlinear bending behavior of bio-inspired composite plates. The inverse hyperbolic shear deformation theory (IHSDT) of plates is employed to characterize the displacement field, with the incorporation of Green-Lagrange nonlinearity. The problem is modeled using the C⁰ finite element method (FEM), and an in-house code is developed in the MATLAB environment to solve it numerically. Various helicoidal layup configurations including helicoidal recursive (HR), helicoidal exponential (HE), helicoidal semi-circular (HS), linear helicoidal (LH), and Fibonacci helicoidal (FH) with different layup sequences and quasi-isotropic configurations are studied. The model is validated, and parametric studies are conducted. These studies investigate the effects of layup configurations, side-to-thickness ratio, modulus ratios, boundary conditions, and loading conditions at different load amplitudes on the nonlinear vibration and nonlinear bending behaviors of bio-inspired composite plates. The results show that the laminate sequence exerts a substantial impact on both nonlinear natural frequencies and nonlinear bending behaviors. Moreover, this influence varies across different side-to-thickness ratios and boundary conditions of the bio-inspired composite plate.

Key words: finite element method (FEM), nonlinear, Green-Lagrange, inverse hyperbolic shear deformation theory (IHSDT), bio-inspired composite plate, helicoidal

中图分类号:

O322

. [J]. Applied Mathematics and Mechanics (English Edition), 2025, 46(1): 81-100.

S. SAURABH, R. KIRAN, D. SINGH, R. VAISH, V. S. CHAUHAN. A comprehensive investigation on nonlinear vibration andbending characteristics of bio-inspired helicoidallaminated composite structures[J]. Applied Mathematics and Mechanics (English Edition), 2025, 46(1): 81-100.

图/表 14

$E 1 / E 2$	$a / h$	$ω max / h$
$E 1 / E 2$	$a / h$	Layup configuration	0.2	0.4	0.6	0.8	1
10	10	HR1	1.044 7	1.181 5	1.382 4	1.428 3	1.535 5
		HR2	1.044 7	1.175 9	1.370 5	1.411 5	1.506 2
		HR3	1.044 7	1.171 7	1.360 8	1.401 7	1.493 2
		HE1	1.044 7	1.182 3	1.384 1	1.436 3	1.553 9
		HE2	1.044 7	1.178 1	1.375 5	1.430 4	1.537 2
		HE3	1.044 7	1.170 3	1.359 0	1.422 7	1.519 8
		HS1	1.044 7	1.143 5	1.302 5	1.498 9	1.450 5
		HS2	1.044 7	1.170 8	1.357 3	1.585 6	1.519 3
		HS3	1.044 7	1.167 5	1.351 3	1.577 3	1.589 1
		LH1	1.044 7	1.176 9	1.372 9	1.418 1	1.513 5
		LH2	1.044 7	1.173 7	1.366 1	1.411 0	1.501 0
		LH3	1.044 7	1.170 4	1.359 1	1.404 7	1.490 9
		FH	1.044 4	1.169 3	1.355 8	1.401 2	1.490 8
		QI	1.042 8	1.162 7	1.340 9	1.559 3	1.573 4

$E 1 / E 2$	$a / h$	$ω max / h$
$E 1 / E 2$	$a / h$	Layup configuration	0.2	0.4	0.6	0.8	1
10	100	HR1	1.030 8	1.140 5	1.298 6	1.497 5	1.483 2
		HR2	1.030 8	1.133 7	1.284 6	1.474 5	1.456 2
		HR3	1.030 8	1.127 4	1.271 5	1.452 8	1.436 0
		HE1	1.030 8	1.141 4	1.300 5	1.500 6	1.495 4
		HE2	1.030 8	1.136 8	1.291 1	1.485 4	1.488 0
		HE3	1.030 8	1.128 3	1.273 5	1.456 6	1.476 2
		HS1	1.030 8	1.100 3	1.215 0	1.360 7	1.529 3
		HS2	1.030 8	1.123 0	1.261 0	1.433 5	1.630 6
		HS3	1.030 8	1.123 8	1.263 0	1.437 3	1.636 8
		LH1	1.030 8	1.135 4	1.288 3	1.480 8	1.469 9
		LH2	1.030 8	1.131 8	1.280 8	1.468 6	1.459 4
		LH3	1.030 8	1.128 1	1.273 0	1.455 8	1.449 4
		FH	1.032 4	1.124 8	1.265 9	1.443 8	1.435 1
		QI	1.030 8	1.118 5	1.252 0	1.419 4	1.610 9

$E 1 / E 2$	$a / h$	$ω max / h$
$E 1 / E 2$	$a / h$	Layup configuration	0.2	0.4	0.6	0.8	1
40	10	HR1	1.074 6	1.285 7	1.262 7	1.488 1	1.489 2
		HR2	1.072 7	1.276 6	1.261 8	1.518 5	1.529 3
		HR3	1.071 9	1.271 0	1.277 8	1.578 5	1.579 5
		HE1	1.074 5	1.285 9	1.273 5	1.482 4	1.501 6
		HE2	1.072 2	1.276 6	1.272 2	1.494 8	1.501 6
		HE3	1.068 0	1.259 1	1.281 5	1.544 5	1.501 6
		HS1	1.054 7	1.205 1	1.271 6	1.327 2	1.501 6
		HS2	1.068 5	1.255 3	1.352 2	1.399 1	1.501 6
		HS3	1.064 1	1.240 8	1.394 7	1.466 4	1.501 6
		LH1	1.072 3	1.276 3	1.254 4	1.496 7	1.501 6
		LH2	1.070 8	1.270 2	1.253 3	1.512 6	1.501 6
		LH3	1.069 4	1.263 9	1.254 5	1.349 4	1.501 6
		FH	1.070 6	1.265 7	1.281 2	1.408	1.599 9
		QI	1.062 4	1.233 2	1.479 3	1.453	1.501 6

$E 1 / E 2$	$a / h$	$ω max / h$
$E 1 / E 2$	$a / h$	Layup configuration	0.2	0.4	0.6	0.8	1
40	100	HR1	1.041 5	1.162 1	1.198 2	1.257 1	1.450 0
		HR2	1.038 8	1.151 0	1.196 7	1.252 9	1.326 8
		HR3	1.036 4	1.141 2	1.201 9	1.260 2	1.334 6
		HE1	1.042 0	1.163 9	1.205 7	1.268 7	1.449 2
		HE2	1.040 3	1.156 8	1.215 9	1.278 1	1.366 1
		HE3	1.037 1	1.144 0	1.310 0	1.295 3	1.364 2
		HS1	1.027 0	1.104 5	1.223 9	1.375 3	1.349 6
		HS2	1.035 5	1.135 9	1.286 8	1.474 0	1.686 6
		HS3	1.035 7	1.136 7	1.289 0	1.478 6	1.694 7
		LH1	1.039 6	1.154 2	1.202 9	1.258 5	1.327 9
		LH2	1.038 1	1.148 4	1.204 8	1.258 3	1.322 3
		LH3	1.036 7	1.142 6	1.207 4	1.259 2	1.320 5
		FH	1.035 5	1.137 6	1.208 8	1.268 6	1.344 1
		QI	1.033 2	1.127 1	1.269 3	1.446 6	1.648 7

$E 1 / E 2$	$a / h$	$ω max / h$
$E 1 / E 2$	$a / h$	Layup configuration	0.2	0.4	0.6	0.8	1
10	10	HR1	1.018 2	1.071 5	1.156 7	1.269 9	1.260 5
		HR2	1.018 1	1.071 1	1.155 7	1.267 5	1.255 3
		HR3	1.018 2	1.071 5	1.156 2	1.267 6	1.257 5
		HE1	1.018 1	1.071 3	1.156 4	1.269 6	1.263 0
		HE2	1.017 9	1.070 5	1.154 5	1.266 1	1.261 2
		HE3	1.017 5	1.068 9	1.150 8	1.259 3	1.258 9
		HS1	1.015 9	1.062 3	1.136 1	1.232 9	1.248 1
		HS2	1.018 5	1.072 5	1.157 6	1.269 9	1.277 4
		HS3	1.017 2	1.067 5	1.147 3	1.252 2	1.377 7
		LH1	1.017 9	1.070 5	1.154 5	1.265 9	1.254 2
		LH2	1.017 8	1.070 0	1.153 2	1.263 5	1.251 5
		LH3	1.017 7	1.069 4	1.152 0	1.261 2	1.249 9
		FH	1.018 1	1.070 9	1.154 8	1.265 1	1.257 4
		QI	1.017	1.066 7	1.145 3	1.248 2	1.260 5

$E 1 / E 2$	$a / h$	$ω max / h$
$E 1 / E 2$	$a / h$	Layup configuration	0.2	0.4	0.6	0.8	1
10	100	HR1	1.010 2	1.040 4	1.089 3	1.155 1	1.235 9
		HR2	1.009 1	1.039 1	1.086 5	1.150 1	1.228 2
		HR3	1.009 6	1.038 0	1.083 8	1.145 5	1.220 9
		HE1	1.010 3	1.040 7	1.090 0	1.156 4	1.237 9
		HE2	1.010 2	1.040 2	1.088 9	1.154 4	1.234 7
		HE3	1.009 9	1.039 2	1.086 6	1.150 3	1.228 3
		HS1	1.008 7	1.034 5	1.076 1	1.131 9	1.200 0
		HS2	1.010 3	1.040 6	1.089 0	1.153 4	1.231 1
		HS3	1.010 1	1.039 9	1.087 7	1.151 3	1.228 5
		LH1	1.010 0	1.039 6	1.087 5	1.152 1	1.231 2
		LH2	1.009 9	1.039 0	1.086 2	1.149 6	1.227 4
		LH3	1.009 7	1.038 3	1.084 7	1.147 0	1.223 4
		FH	1.009 5	1.037 6	1.083 1	1.144 2	1.219 0
		QI	1.010 0	1.039 3	1.086 3	1.148 9	1.224 5

$E 1 / E 2$	$a / h$	$ω max / h$
$E 1 / E 2$	$a / h$	Layup configuration	0.2	0.4	0.6	0.8	1
40	10	HR1	1.038 9	1.153 5	1.171 2	1.227 4	1.353 4
		HR2	1.039 5	1.154 9	1.176	1.237 1	1.398 7
		HR3	1.040 5	1.157 2	1.190 8	1.260 5	1.457 9
		HE1	1.038 3	1.151 3	1.171 8	1.201 1	1.345 4
		HE2	1.037 6	1.148 2	1.172 7	1.351 1	1.356 9
		HE3	1.036 0	1.141 5	1.177 7	1.245 1	1.390 7
		HS1	1.030 9	1.119 8	1.181 7	1.218 5	1.263 4
		HS2	1.037 4	1.144 8	1.209 3	1.238 0	1.267 2
		HS3	1.031 9	1.124 3	1.268 6	1.269 9	1.300 4
		LH1	1.038 5	1.151 5	1.167 7	1.214 3	1.376 9
		LH2	1.038 4	1.150 6	1.168 6	1.215 9	1.389 3
		LH3	1.038 2	1.149 6	1.712 0	1.219 8	1.412 4
		FH	1.039 8	1.154 3	1.191 4	1.258 7	1.474 8
		QI	1.032 1	1.124 2	1.266 4	1.261 6	1.294 5

$E 1 / E 2$	$a / h$	$ω max / h$
$E 1 / E 2$	$a / h$	Layup configuration	0.2	0.4	0.6	0.8	1
40	100	HR1	1.010 7	1.042 7	1.096 4	1.092 6	1.117 5
		HR2	1.010 2	1.040 8	1.091 7	1.091 4	1.114 3
		HR3	1.009 8	1.039 0	1.087 2	1.094 4	1.117 9
		HE1	1.010 8	1.043 2	1.097 6	1.095 8	1.122 9
		HE2	1.010 6	1.042 4	1.095 5	1.099 9	1.125 8
		HE3	1.010 2	1.040 8	1.091 3	1.111 0	1.135 7
		HS1	1.008 5	1.003 6	1.074 3	1.129 3	1.196 7
		HS2	1.010 8	1.042 5	1.093 2	1.160 2	1.241 1
		HS3	1.010 4	1.041 2	1.090 6	1.156 3	1.236 0
		LH1	1.010 4	1.041 6	1.093 5	1.093 9	1.117 0
		LH2	1.010 2	1.040 6	1.091 2	1.094 6	1.116 7
		LH3	1.009 9	1.039 6	1.088 8	1.096 0	1.117 3
		FH	1.009 7	1.038 5	1.086 0	1.097 9	1.122 2
		QI	1.010 3	1.040 5	1.088 9	1.153 2	1.230 8

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