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Frontiers of Mechanical Engineering

ISSN 2095-0233

ISSN 2095-0241(Online)

CN 11-5984/TH

Postal Subscription Code 80-975

2018 Impact Factor: 0.989

Front. Mech. Eng.    2020, Vol. 15 Issue (4) : 571-584    https://doi.org/10.1007/s11465-020-0592-4
RESEARCH ARTICLE
Influence factors on natural frequencies of composite materials
Bo WANG, Feng ZHAO, Zixu ZHAO, Kunpeng XU()
School of Mechanical Engineering and Automation, Northeastern University, Shenyang 110819, China; Key Laboratory of Vibration and Control of Aero-Propulsion Systems (Ministry of Education), Northeastern University, Shenyang 110819, China
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Abstract

Compared with traditional materials, composite materials have lower specific gravity, larger specific strength, larger specific modulus, and better designability structure and structural performance. However, the variability of structural properties hinders the control and prediction of the performance of composite materials. In this work, the Rayleigh–Ritz and orthogonal polynomial methods were used to derive the dynamic equations of composite materials and obtain the natural frequency expressions on the basis of the constitutive model of laminated composite materials. The correctness of the analytical model was verified by modal hammering and frequency sweep tests. On the basis of the established theoretical model, the influencing factors, including layers, thickness, and fiber angles, on the natural frequencies of laminated composites were analyzed. Furthermore, the coupling effects of layers, fiber angle, and lay-up sequence on the natural frequencies of composites were studied. Research results indicated that the proposed method could accurately and effectively analyze the influence of single and multiple factors on the natural frequencies of composite materials. Hence, this work provides a theoretical basis for preparing composite materials with different natural frequencies and meeting the requirements of different working conditions.

Keywords composite material      hammering and frequency sweep test      structural parameter      natural frequency     
Corresponding Author(s): Kunpeng XU   
Just Accepted Date: 30 July 2020   Online First Date: 11 September 2020    Issue Date: 02 December 2020
 Cite this article:   
Bo WANG,Feng ZHAO,Zixu ZHAO, et al. Influence factors on natural frequencies of composite materials[J]. Front. Mech. Eng., 2020, 15(4): 571-584.
 URL:  
https://academic.hep.com.cn/fme/EN/10.1007/s11465-020-0592-4
https://academic.hep.com.cn/fme/EN/Y2020/V15/I4/571
Fig.1  Production process of fiber-reinforced composites.
E1 E2 ν12 G12 ρ Layer angle
33.5 GPa 4.5 GPa 0.3 5 GPa 1600 kg/m3 0°/90°/0°
Tab.1  Composite structural parameter values and material parameter values
Fig.2  Modal test chart of composite material.
Fig.3  Simplified diagram of the distribution of laser reflection strips.
i Test frequency, ωi*/Hz Test mode shape Theoretical frequency, ωi/Hz Theory mode shape Error, ωi*ω i ωi */%
1 292.195 298.457 −2.140
2 810.355 792.698 2.179
3 1874.250 1894.750 −1.094
4 2531.530 2548.850 −0.684
Tab.2  Comparison of mode shapes and natural frequencies from theoretical calculation and experimental test
Fig.4  Laminated composite materials with different structures.
Length Width Thickness Number of layers Thickness of each layer
80 mm 50 mm 3 mm n 3/n mm
Tab.3  Structural parameters of composite materials with different layers
Fig.5  Effect of the number of layers on the natural frequencies of composites.
Fig.6  Effect of odd and even numbers of layers on the natural frequencies of composite materials. (a) Odd-numbered layers; (b) even-numbered layers.
Length Width Thickness Thickness of each layer Layer angle
80 mm 50 mm 1 × n mm 1 mm 0°/90°/0°/90°/0°/90°/⋯
Tab.4  Structural parameters of composite materials with different thicknesses
Fig.7  Variation of natural frequencies of materials with thickness.
Length Width Thickness Layer Layer angle
80 mm 50 mm 3 mm 1 θ°
Tab.5  Structural parameters of composite materials with different angles
Fig.8  Variation of natural frequencies of materials with layer angle.
Length Width Thickness Layers Thickness of each layer
80 mm 50 mm 3 mm 2 1.5 mm
Tab.6  Structural parameters of composite materials with different relative angles
Fig.9  Variation of natural frequencies of materials with relative layer angle.
Length Width Thickness Layers Thickness of each layer
80 mm 50 mm 3 mm n 3/n mm
Tab.7  Structural parameters of composite materials with different structures
Fig.10  Laminated composite materials with different structures.
Fig.11  Effects of different structures on the first-order natural frequency. (a) 2D curve graph; (b) 3D histogram.
Fig.12  Effects of different structures on the second-order natural frequency. (a) 2D curve graph; (b) 3D histogram.
Fig.13  Effects of different structures on the third-order natural frequency. (a) 2D curve graph; (b) 3D histogram.
Fig.14  Effects of different structures on the fourth-order natural frequency. (a) 2D curve graph; (b) 3D histogram.
Fig.15  Effects of the number of layers on the natural frequencies of different structures. (a) SY1; (b) SY2; (c) OB1; (d) OB2; (e) QI.
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