On the vibration and stability behaviors of heterogeneous-CNTRC-truncated conical shells under axial load in the context of FSDT

被引:45
作者
Sofiyev, A. H. [1 ]
机构
[1] Fac Suleyman Demirel Univ, Dept Civil Engn Engn, Isparta 32260, Turkey
关键词
Nanocomposites; Vibration; Stability; HT-CNTRC; Truncated cone; Axial load; NANOTUBE-REINFORCED COMPOSITES; CYLINDRICAL-SHELLS; BUCKLING ANALYSIS; CARBON NANOTUBES; NANOCOMPOSITES; COMPRESSION; PRESSURE;
D O I
10.1016/j.tws.2020.106747
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
The vibration and stability of heterogenous (HT) carbon nanotube reinforced composite truncated conical shells (HT-CNTRC-TCSs) are studied. The main feature of this study is to expand the first order shear deformation theory to the HT-CNTRC-TCSs to obtain an analytical solution of vibration and stability problems. The dynamic stability equations of HT-CNTRC-TCSs are solved by applying Galerkin method. The expressions for the frequency and the critical axial load of HT-CNTRC-TCSs are obtained. In numerical calculations, the influences of heterogeneity and volume fraction of CNTs on the frequency and critical axial load of HT-CNTRC-TCSs are studied in detail.
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页数:11
相关论文
共 34 条
[1]  
Ambartsumian S.A., 1961, Theory of Anisotropic Shells
[2]  
[Anonymous], ENG STRUCT
[3]   Buckling analysis of axially-loaded functionally graded carbon nanotube-reinforced composite conical panels using a novel numerical variational method [J].
Ansari, Reza ;
Torabi, Jalal ;
Shojaei, Mostafa Faghih ;
Hasrati, Emad .
COMPOSITE STRUCTURES, 2016, 157 :398-411
[4]   Numerical study on the buckling and vibration of functionally graded carbon nanotube-reinforced composite conical shells under axial loading [J].
Ansari, Reza ;
Torabi, Jalal .
COMPOSITES PART B-ENGINEERING, 2016, 95 :196-208
[5]   Two-dimensional thermo-elastic analysis of FG-CNTRC cylindrical pressure vessels [J].
Arefi, Mohammad ;
Mohammadi, Masoud ;
Tabatabaeian, Ali ;
Dimitri, Rossana ;
Tornabene, Francesco .
STEEL AND COMPOSITE STRUCTURES, 2018, 27 (04) :525-536
[6]   Dynamic stability analysis of a pressurized FG-CNTRC cylindrical shell interacting with supersonic airflow [J].
Asadi, Hamed ;
Wang, Quan .
COMPOSITES PART B-ENGINEERING, 2017, 118 :15-25
[7]   Carbon nanotube-reinforced composites as structural materials for microactuators in microelectromechanical systems [J].
Ashrafi, Behnam ;
Hubert, Pascal ;
Vengallatore, Srikar .
NANOTECHNOLOGY, 2006, 17 (19) :4895-4903
[8]   Investigation for electro-thermo-mechanical vibration of nanocomposite cylindrical shells with an internal fluid flow [J].
Dinh Gia Ninh ;
Nguyen Duc Tien .
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 92 :501-519
[9]   Characteristics of nonlinear vibration of nanocomposite cylindrical shells with piezoelectric actuators under thermo-mechanical loads [J].
Dinh Gia Ninh ;
Dao Huy Bich .
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 77 :595-609
[10]   Nonlinear thermal torsional post-buckling of carbon nanotube-reinforced composite cylindrical shell with piezoelectric actuator layers surrounded by elastic medium [J].
Dinh Gia Ninh .
THIN-WALLED STRUCTURES, 2018, 123 :528-538