Applied Mathematics and Mechanics >
Vibration and response behaviors of composite sandwich cylindrical shells with a carbon nanotube-reinforced damping gel honeycomb core
Received date: 2025-07-01
Revised date: 2025-08-20
Online published: 2025-09-30
Supported by
Project supported by the National Natural Science Foundation of China (Nos. 12472005 and 52175079), the Aerospace Science Foundation of China (No. 2022Z009050002), the Key Laboratory of Vibration and Control of Aero-Propulsion System, Ministry of Education of China (No. VCAME201603), and the Tai-Hang Laboratory Program (No. AK023)
Copyright
This study provides a thorough investigation into the vibration behavior and impulse response characteristics of composite honeycomb cylindrical shells filled with damping gel (DG-FHCSs). To address the limitations of existing methods, a dynamic model is developed for both free and forced vibration scenarios. These models incorporate the virtual spring technology to accurately simulate a wide range of boundary conditions. Using the first-order shear deformation theory in conjunction with the Jacobi orthogonal polynomials, an energy expression is formulated, and the natural frequencies and mode shapes are determined via the Ritz method. Based on the Newmark-
Peiyao XU , Zhuo XU , Shang GENG , Hui LI , Yan ZHOU , Haijun WANG , Jian XIONG , Zeng LIN , Jun LI . Vibration and response behaviors of composite sandwich cylindrical shells with a carbon nanotube-reinforced damping gel honeycomb core[J]. Applied Mathematics and Mechanics, 2025 , 46(10) : 1867 -1882 . DOI: 10.1007/s10483-025-3304-7
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