Active vibration control of composite shallow shells: An integrated approach

Authors

  • N. Rahman Department of Mechanical Engineering, Zakir Husain College of Engineering and Technology, Aligarh Muslim University, Aligarh, U.P-202002, India
  • M.N. Alam Department of Mechanical Engineering, Zakir Husain College of Engineering and Technology, Aligarh Muslim University, Aligarh, U.P-202002, India
  • M. Junaid Department of Mechanical Engineering, Zakir Husain College of Engineering and Technology, Aligarh Muslim University, Aligarh, U.P-202002, India

DOI:

https://doi.org/10.15282/jmes.12.1.2018.6.0300

Keywords:

Shell; composite; finite element modeling; ABAQUS; constant gain velocity feedback; linear quadratic regulator.

Abstract

Active vibration control of smart composite shallow shells with distributed piezoelectric sensors and actuators is presented in this work. An integrated approach is used for recording the uncontrolled and controlled vibration response under pressure impulse load. The FE model developed in ABAQUS is utilized to generate the global mass, stiffness and load matrices of the system. The system matrices are arranged in statespace format and the dynamic equations of the system are obtained. The controlled responses are achieved using the inputs from FE model in ABAQUS in conjunction with the developed MATLAB codes for Constant Gain Velocity Feedback (CGVF) and Linear Quadratic Regulator (LQR) control strategies. The method is first validated by comparing the natural frequencies obtained using the ABAQUS generated matrices with that obtained using an FE model with four noded quadrilateral shallow shell element based on efficient zigzag theory. The shell element uses the concept of electric nodes to satisfy the equipotential condition of electrode surface. An 8-noded linear piezoelectric brick element is used for piezoelectric layers and an 8-noded quadrilateral continuum shell element is used for the elastic layers of hybrid shells for making the finite element mesh in ABAQUS. The non-dimensional natural frequencies and active vibration control responses for hybrid composite cylindrical and spherical shells are presented for clamped-clamped and cantilever boundary conditions. Boundary conditions have significant effect on vibration amplitude, control voltage and settling time. In comparison to CGVF controller, a better control in lesser time is achieved with LQR controller for a shell with similar boundary conditions. Larger gain values (G) are required for vibration control of thick shells.

References

Qian W, Liu GR, Chun L, & Lam KY. Active vibration control of composite laminated cylindrical shells via surface-bonded magnetostrictive layers. Smart Materials & Structures. 2003;12(6):889-897

Bhattacharya P, Suhail H & Sinha PK. Finite element analysis and distributed control of laminated composite shells using LQR/IMSC approach. Aerospace Science and Technology. 2002; 6:273–281.

Balamurugan V & Narayanan S. A piezolaminated composite degenerated shell finite element for active control of structures with distributed piezosensors and actuators. Smart Materials & Structures.2008; 17(3):1–18.

Ray M. C. Optimal control of laminated shells using piezoelectric sensor and actuator layers. AIAA Journal. 2003; 41(6):1151-1157.

Kapuria S & Yasin MY. Coupled efficient layerwise finite element modeling for active vibration control of smart composite and sandwich shallow shells. Journal of Intelligent Material Systems and Structures. 2014; 25(16):2013-2036.

Ray MC & Reddy JN. Optimal control of thin circular cylindrical laminated composite shells using active constrained layer damping treatment. Smart Materials & Structures. 2004; 13(1): 64-72.

Kumar DN, Raja S & Ikeda T. Active vibration control of smart plates with partially debonded multi-layered PZT actuators. Smart Mater Struct. 2007; 16: 1584-1594.

Zhang YH, Xie SL & Zhang XN. Vibration control of a simply supported cylindrical shell using a laminated piezoelectric actuator. Acta Mechanica. 2008; 196(1-2): 87-101.

Rahman N & Alam MN. Active vibration control of a piezoelectric beam using PID controller: Experimental study. Latin American Journal of Solids and Structures.2012; 9(6):657-673.

Li HY, Lin QY, Liu ZX & Wang C. Active control of the piezoelastic laminated cylindrical shell's vibration under hydrostatic pressure. Applied Mathematics and Mechanics-English Edition. 2003; 24(2):182-195.

Kapuria S & Yasin MY. Active vibration control of piezoelectric laminated beams with electroded actuators and sensors using an efficient finite element involving an electric node. Smart Materials and Structures. 2010; 19(4). doi: Artn 045019.

Lee SJ and Reddy JN Vibration suppression of laminated shell structures investigated using higher order shear deformation theory. Smart Materials & Structures. 2004; 13(5):1176-1194.

Rahman N and Alam MN. Active Vibration Suppression of Piezoelectric Laminated Beam based on Efficient Finite Element Model using LQG Controller. International Journal of Theoretical and Applied Mechanics. 2012; 7(1): 9-24.

Rahman N and Alam MN. Structural Control of Piezoelectric Laminated Beams under Thermal Load. Journal of Thermal Stresse.2015; 38: 69–95.

Moita JMS, Correia IFP, Soares CMM & Soares CAM. Active control of adaptive laminated structures with bonded piezoelectric sensors and actuators. Computers & Structures. 2004; 82(17-19): 1349-1358.

Ray MC & Mallik N. Active control of laminated composite beams using a piezoelectric fibre reinforced composite layer. Smart Mater Struct. 2004; 13: 146-152.

Pradhan SC & Reddy JN. Vibration control of composite shells using embedded actuating layers. Smart Materials & Structures.2004; 13(5): 1245-1257.

Ray MC & Batra RC. Smart constrained layer damping of functionally graded shells using vertically/obliquely reinforced 1-3 piezocomposite under a thermal environment. Smart Materials Structures. 2008; 17(5). doi: Artn 055007 10.1088/0964-1726/17/5/055007

Zhang YH, Zhang XN & Xie SL. Adaptive vibration control of a cylindrical shell with laminated PVDF actuator. Acta Mechanica. 2010; 210(1-2): 85-98.

Sarangi SK & Ray MC. Smart control of nonlinear vibrations of doubly curved functionally graded laminated composite shells under a thermal environment using 1-3 piezoelectric composites. International Journal of Mechanics and Materials in Design. 2013; 9(3): 253-280.

Neto MA, Ambrosio JAC, Roseiro LM, Amaro A & Vasques CMA. Active vibration control of spatial flexible mutibody systems. Multibody Syst Dyn.2013; 30(1):13-35.

Hua-ping T, Yun-jun T & Gong-an T. Active vibration control of mutibody system with quick startup and brake based on active damping. J Cent South Univ T. 2006; 13(4): 417- 421.

Song ZG & Li FM. Active aeroelastic flutter analysis and vibration control of supersonic composite laminated plate. Composite Structures. 2012; 94(2): 702-713.

Shah PH & Ray MC. Active control of laminated composite truncated conical shells using vertically and obliquely reinforced 1-3 piezoelectric composites. European Journal of Mechanics a-Solids. 2012; 32: 1-12.

Sarangi SK & Ray MC. Active damping of geometrically nonlinear vibrations of doubly curved laminated composite shells. Composite Structures. 2011; 93(12):3216-3228.

Sun BH & Huang D. Vibration suppression of laminated composite beams with a piezo-electric damping layer. Composite Structures. 2001; 53(4): 437-447.

Zhang HY & Shen YP. Vibration suppression of laminated plates with 1-3 piezoelectric fiber-reinforced composite layers equipped with interdigitated electrodes. Composite Structures. 2007; 79(2): 220-228.

Baillargeon BP, Vel SS & Koplik JS. Utilizing ABAQUS to Analyze the Active Vibration Suppression of Structural Systems. Paper presented at the ABAQUS Users’Conference, Boston, MA USA. 2004.

Vasques CMA & Rodrigues JD. Active vibration control of smart piezoelectric beams: Comparison of classical and optimal feedback control strategies. Computers & Structures. 2006; 84(22-23): 1402-1414.

Balamurugan V & Narayanan S. Shell finite element for smart piezoelectric composite plate/shell structures and its application to the study of active vibration control. Finite Elem Anal Des. 2001; 37(9): 713-738.

Roy T & Chakraborty D. (2009). Optimal vibration control of smart fiber reinforced composite shell structures using improved genetic algorithm. Journal of Sound and Vibration. 2009; 319(1-2): 15-40. doi: 10.1016/j.jsv.2008.05.037

Bailey T & Hubbard JE (1985). Distributed Piezoelectric Polymer Active Vibration Control of a Cantilever Beam. Journal of Guidance Control and Dynamics. 1985; 8(5): 605-611. doi: Doi 10.2514/3.20029

Kim SJ, Hwang JS & Mok J. Active vibration control of composite shell structure using modal Sensor/Actuator system. KSAS International Journal. 2006; 7(1): 106-117.

Sun L, Li W, Wu Y and Lan Q. Active vibration control of a conical shell using piezoelectric ceramics. Journal of Low Frequency Noise,Vibration and Active Control. 2017; 36(4): 366–375

Loghmani A, Danesh M, Keshmiri M and Savadi MM. Theoretical and experimental study of active vibration control of a cylindrical shell using piezoelectric disks. Journal of Low Frequency Noise,Vibration and Active Control. 2015; 34(3): 269 – 288

He J and Chen X. Integrated topology optimization of structure/vibration control for piezoelectric cylindrical shell based on the genetic algorithm. Shock and Vibration. 2015; 2015: 10. doi: 10.1155/2015/456147.

Published

2018-03-31

How to Cite

[1]
N. Rahman, M. Alam, and M. Junaid, “Active vibration control of composite shallow shells: An integrated approach”, J. Mech. Eng. Sci., vol. 12, no. 1, pp. 3354–3369, Mar. 2018.

Similar Articles

<< < 23 24 25 26 27 28 29 30 31 32 > >> 

You may also start an advanced similarity search for this article.