Smart damping of functionally graded nanotube reinforced composite rectangular plates

被引:41
作者
Sharma, Anshul [1 ,2 ]
Kumar, Anuruddh [1 ]
Susheel, C. K. [1 ]
Kumar, Rajeev [1 ]
机构
[1] Indian Inst Technol, Sch Engn, Mandi 175001, Himachal Prades, India
[2] Natl Inst Technol, Dept Mech Engn, Hamirpur 177005, Himachal Prades, India
关键词
Functionally graded carbon nanotube reinforced composite; Active vibration control; Space antenna reflector; Piezoelectric ceramics; Thermal shock; Finite element formulation; Nonlinear fuzzy logic controller; ACTIVE VIBRATION CONTROL;
D O I
10.1016/j.compstruct.2016.07.079
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
In this study, the dynamic response and the active vibration control behavior of various functionally graded carbon nanotube reinforced composite (FGCNTRC) rectangular plates is investigated numerically instrumented with piezoelectric sensor and actuator layers. The functionally graded plate is modeled using finite element method incorporating first order shear deformation theory is implemented in order to predict static and dynamic responses of vibrating structure. The linear piezoelectric theory is implemented to model the piezoelectric effect across the thickness. The equations of motion of the smart plate are formulated using Hamilton's principle. The nonlinear fuzzy logic controller is designed as multi input single output (MISO) system using 49 If-Then rules and implemented numerically to perform active vibration control. The results are presented both in the time domain and frequency domain. The numerical simulations conclude that the FG-O plate panel demonstrates the fastest vibration attenuation subjected to impact load using a fuzzy logic controller followed by FG-V, FG-UD and FG-X plate panels irrespective of volume fraction of the CNTs as well as boundary conditions. The effect of temperature rise and volume fraction of CNT on natural frequency of CNT reinforced composite plate with different boundary conditions is also investigated. (C) 2016 Elsevier Ltd. All rights reserved.
引用
收藏
页码:29 / 44
页数:16
相关论文
共 44 条
[1]   ALIGNED CARBON NANOTUBE ARRAYS FORMED BY CUTTING A POLYMER RESIN-NANOTUBE COMPOSITE [J].
AJAYAN, PM ;
STEPHAN, O ;
COLLIEX, C ;
TRAUTH, D .
SCIENCE, 1994, 265 (5176) :1212-1214
[3]  
Andoh FH, 2004, J INTEL MAT SYST STR, V15, P3, DOI 10.1177/1045389X01039262
[4]  
[Anonymous], 2006, FINITE ELEMENT PROCE
[5]   Vibrational analysis of carbon nanotube-reinforced composite quadrilateral plates subjected to thermal environments using a weak formulation of elasticity [J].
Ansari, R. ;
Shahabodini, A. ;
Shojaei, M. Faghih .
COMPOSITE STRUCTURES, 2016, 139 :167-187
[6]   Nonlinear analysis of forced vibration of nonlocal third-order shear deformable beam model of magneto-electro-thermo elastic nanobeams [J].
Ansari, R. ;
Hasrati, E. ;
Gholami, R. ;
Sadeghi, F. .
COMPOSITES PART B-ENGINEERING, 2015, 83 :226-241
[7]   Size-dependent nonlinear forced vibration analysis of magneto-electro-thermo-elastic Timoshenko nanobeams based upon the nonlocal elasticity theory [J].
Ansari, R. ;
Gholami, R. ;
Rouhi, H. .
COMPOSITE STRUCTURES, 2015, 126 :216-226
[8]   Nonlinear forced vibration analysis of functionally graded carbon nanotube-reinforced composite Timoshenko beams [J].
Ansari, R. ;
Shojaei, M. Faghih ;
Mohammadi, V. ;
Gholami, R. ;
Sadeghi, F. .
COMPOSITE STRUCTURES, 2014, 113 :316-327
[9]   Evaluation of effective elastic properties of layered composite fiber-reinforced plastic plates by piezoelectrically induced guided waves and laser Doppler vibrometry [J].
Eremin, A. A. ;
Glushkov, E. V. ;
Glushkova, N. V. ;
Lammering, R. .
COMPOSITE STRUCTURES, 2015, 125 :449-458
[10]   Thermo-mechanical properties of randomly oriented carbon/epoxy nanocomposites [J].
Fidelus, JD ;
Wiesel, E ;
Gojny, FH ;
Schulte, K ;
Wagner, HD .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2005, 36 (11) :1555-1561