Abstract
Bi-stable composite laminated structure was a composite laminated structure with two different steady-state characteristics, which could be kept in two steady states without the maintenance of external loads. In this paper, the dynamic governing equation of bi-stable cross-ply carbon fiber-reinforced composite laminates under foundation excitation is established by using Hamilton's principle, taking into account geometric nonlinearity. Newton–Raphson method is used to solve the equilibrium point, and the effect of curing temperature on the steady-state configuration of bi-stable laminates is studied. The equations are numerically simulated by using Runge–Kutta method, which allows the nonlinear dynamic response curve of the system to be obtained, and the dynamic jump analysis of the bi-stable laminates is carried out.
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Acknowledgements
The authors gratefully acknowledge the supports of National Natural Science Foundation of China (NNSFC) through Grant Nos. 12002057 and 11832002, Scientific Research Project of Beijing Educational Committee No. KM202111232023, Qin Xin Talents Cultivation Program, Beijing Information Science and Technology University QXTCP C202102.
Funding
Natural Science Foundation of China (NNSFC) through Grant Nos. 12002057 and 11832002; Scientific Research Project of Beijing Educational Committee No. KM202111232023; Qin Xin Talents Cultivation Program, Beijing Information Science and Technology University QXTCP C202102.
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Yang, S.W., Wang, Z.Q. & Zhang, W. Dynamic jump analysis of Bi-stable square plate under foundation excitation. Int. J. Dynam. Control 10, 1760–1769 (2022). https://doi.org/10.1007/s40435-022-00958-w
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DOI: https://doi.org/10.1007/s40435-022-00958-w