Abstract
Thin cylindrical shells are susceptible to cracking under long-term load and external impact, and it is of considerable scientific and technical value to investigate the nonlinear vibration response characteristics and monitor the health condition of the shell structure. Based on the Flügge shell theory, the nonlinear dynamic model for the thin cylindrical shell is established. By the partial Fourier transform combined with the residue theorem, the forced vibration generation and propagation mechanism of the thin cylindrical shell are investigated, and the analytical solution of forced vibration displacement in the space domain is obtained. Then, the local flexibility matrix is derived from the perspective of fracture mechanics, and the continuous coordination condition on both sides of the straight crack is constructed using the linear spring model. Combined with the wave superposition principle, the analytical approach for nonlinear vibration response is proposed to reveal the evolution law of vibration characteristics of the thin cylindrical shell with a straight crack, and then, a straight crack identification method based on natural frequency isolines and amplitude maximization methods is presented. Finally, the effect of various morphological information of the straight crack on the nonlinear vibration response characteristics of the thin cylindrical shell is studied in detail, and a numerical case is conducted to verify the effectiveness of the proposed straight crack identification method.
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Funding
This research was funded by National Natural Science Foundation of China (Grant Nos. 51775501 and 52175124), Natural Science Foundation of Zhejiang province (Grant Nos. LZ21E050003 and LY17E050004) and Zhejiang Provincial Science and Technology Innovation Activity Program for College Students (New Miao Talent Program) (Grant No. 2021R403064)
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TW was involved in the conceptualization, methodology, software, formal analysis, validation, data curation, writing—original draft preparation, writing—review and editing. CW contributed to the validation, investigation, resources, and visualization. YY was involved in the validation, data curation, and writing—original draft preparation. YZ assisted in the formal analysis, investigation, and visualization. LL contributed to the investigation, visualization. DT was involved in the conceptualization, methodology, project administration, and funding acquisition.
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Appendices
Appendix A
The detailed expressions of coefficient matrix \(\left[ {N_{3 \times 3} } \right]\) are described in the following forms.
Appendix B
The coefficient \(a_{i} \left( {i = 0,2,4,6,8} \right)\) of the algebraic equation in Sect. 2.1 are expressed as
Appendix C
The analytical solutions of axial \(u(x)\), circumferential \(v(x)\), and radial \(w(x)\) displacement responses are obtained using the residue theorem.
where \(\alpha^{\prime}_{1}\), \(\beta^{\prime}_{1}\) \(\gamma^{\prime}_{1}\), \(\alpha^{\prime}_{2}\), \(\beta^{\prime}_{2}\), \(\gamma^{\prime}_{2}\), \(\alpha^{\prime}_{3}\), \(\beta^{\prime}_{3}\), \(\gamma^{\prime}_{3}\), \(a^{\prime}_{8}\), \(a^{\prime}_{6}\), \(a^{\prime}_{4}\), and \(a^{\prime}_{2}\) are coefficient, which are given as:
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Wang, T., Wang, C., Yin, Y. et al. Analytical approach for nonlinear vibration response of the thin cylindrical shell with a straight crack. Nonlinear Dyn 111, 10957–10980 (2023). https://doi.org/10.1007/s11071-023-08460-4
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DOI: https://doi.org/10.1007/s11071-023-08460-4