Dynamic response of rotating beams with piezoceramic actuation

Journal of Sound and Vibration

Volumn 270, Issue 4-5, 2004, Pages 729-753

  Thakkar, Dipali ^a   Ganguli, Ranjan ^a  

^a INDIAN INSTITUTE OF SCIENCE   (India)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; BENDING (DEFORMATION); DYNAMIC RESPONSE; FINITE ELEMENT METHOD; HAMILTONIANS; NONLINEAR EQUATIONS; NUMERICAL METHODS; TORSION TESTING;

INPLANE BENDING; PIEZOCERAMIC ACTUATION; ROTATING BEAMS; TRANSVERSE BENDING;

VIBRATIONS (MECHANICAL);

EID: 1442265967     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0022-460X(03)00189-5     Document Type: Article

References (38)

1. E. Crawley, Intelligent structures for aerospace: a technology overview and assessment, American Institute of Aeronautics and Astronautics Journal 32 (1994) 1689-1699.
2. V. Giurgiutiu, Review of smart-materials actuation solutions for aeroelastic and vibration control, Journal of Intelligent Material Systems and Structures 11 (2000) 525-543.
3. I. Chopra, Status of application of smart structures technology to rotorcraft systems, Journal of American Helicopter Society 45 (2000) 228-252.
4. C. Wang, K. Ang, A. Ajit, Shape control of laminated cantilevered beams with piezoceramic actuators, Journal of Intelligent Material Systems and Structures 10 (1999) 164-175.
5. D. Robbins, J. Reddy, Analysis of piezoelectrically actuated beams using a layer-wise displacement theory, Journal of Computers and Structures 41 (1990) 265-279.
6. N. Lobontiu, M. Goldfarb, E. Garcia, Achieving maximum tip displacement during resonant excitation of piezoelectrically actuated beams, Journal of Intelligent Material Systems and Structures 10 (1999) 900-913.
7. D. Huang, B. Sun, Approximate analytical solutions of smart composite mindlin beams, Journal of Sound and Vibration 244 (2001) 379-394.
8. M. Friswell, On the design of modal actuators and sensors, Journal of Sound and Vibration 241 (2001) 361-372.
9. D. Sun, L. Tong, Sensor/actuator equations for curved piezoelectric fibers and vibration control of composite beams using fiber modal actuators/sensors, Journal of Sound and Vibration 241 (2001) 297-314.
10. L. Librescu, L. Meirovitch, S. Na, Control of cantilever vibration via structural tailoring and adaptive materials, American Institute of Aeronautics and Astronautics Journal 35 (1997) 1309-1315.
11. P. Chen, I. Chopra, Hover testing of smart rotor with induced-strain actuation of blade twist, American Institute of Aeronautics and Astronautics Journal 35 (1997) 6-16.
12. S. Rao, R. Gupta, Finite element vibration analysis of rotating Timoshenko beams, Journal of Sound and Vibration 242 (2001) 103-124.
13. S. Lin, K. Hsio, Vibration analysis of a rotating Timoshenko beam, Journal of Sound and Vibration 240 (2001) 303-322.
14. D. Diker, Vibration control of a rotating Euler-Bernoulli beam, Journal of Sound and Vibration 232 (2000) 541-551.
15. J. Chung, H. Yoo, Dynamic analysis of a rotating cantilever beam by using the finite element method, Journal of Sound and Vibration 249 (2002) 147-164.
16. D. Hodges, Y. Chung, X. Shang, Discrete transfer matrix method for non-uniform rotating beams, Journal of Sound and Vibration 240 (1994) 276-283.
17. A. Chattopadhyay, H. Gu, Q. Lin, Modeling of smart composite box beams with nonlinear induced strain, Journal of Composites 30 (B) (1999) 603-612.
18. C. Cesnik, S. Shin, On the twist performance of a multiple-cell active helicopter blade, Journal of Smart Materials and Structures 10 (1999) 53-61.
19. A. Baz, J. Rao, Vibration control of rotating beams with active constrained layer damping, Journal of Smart Materials and Structures 10 (2000) 112-120.
20. D. Hodges, E. Dowell, Non-linear equations of motion for the elastic bending and torsion of twisted nonuniform rotor blades, NASA TN D-7818, 1974.
21. I. Chopra, T. Sivaneri, Aeroelastic stability of rotor blades using finite element analysis, NASA CR 166389, 1982.
22. E. Smith, Vibration and flutter of stiff-inplane elastically tailored composite rotor blades, Journal of Mathematical and Computer Modeling, Special Edition on Rotorcraft Modeling, No 1 and 2 20 (1994).
23. R. Ganguli, I. Chopra, Aeroelastic optimization of a helicopter rotor using two-cell composite blades, American Institute of Aeronautics and Astronautics Journal 34 (1996) 835-841.
24. P. Inthra, F. Gandhi, Optimal control of helicopter vibration through cyclic variations in blade root stiffness, Journal of Smart Materials and Structures 10 (2001) 96-103.
25. P. Friedmann, Rotary wing aeroelasticity with application to VTOL vehicles, Proceedings of the 31st AIAA/ASME/ASCE/ASC Structures, Structural Dynamics and Materials Conference, Long Beach, CA, April 2-4, 1990, pp. 1624-1667.
26. A. Benjeddou, M. Trindade, R. Ohayon Piezoelectric actuation mechanisms for intelligent sandwich structures, Journal of Smart Materials and Structures 9 (1999) 328-335.
27. C. Sun, X. Zhang, Use of thickness-shear mode in adaptive sandwich structures, Journal of Smart Materials and Structures 4 (1995) 202-206.
28. A. Benjeddou, M. Trindade, R. Ohayon, New shear actuated smart structure beam finite element, American Institute of Aeronautics and Astronautics Journal 37 (1999) 378-383.
29. W. Chen, A. Saleeb, Constitutive Equations for Engineering Materials, Vol. 1: Elasticity and Modeling, Wiley-Interscience, USA, 1952.
30. C. Lin, C. Hsu, H. Huang, Finite element analysis on deflection control of plates with piezoelectric actuators, Journal of Composite Structures 35 (1996) 423-433.
31. J. Epps, R. Chandra, The natural frequencies of rotating composite beams with tip sweep, Journal of American Helicopter Society 41 (1996) 29-36.
32. R. Ganguli, I. Chopra, W. Weller, Comparison of calculated vibratory rotor hub loads with experimental data, Journal of American Helicopter Society 43 (1998) 312-318.
33. R. Ganguli, Optimum design of a helicopter rotor for low vibration using aeroelastic analysis and response surface model, Journal of Sound and Vibration 258 (2002) 327-344.
34. C. Park, C. Walz, I. Chopra, Bending and torsion models of beams with induced-strain actuators, Journal of Smart Materials and Structures 5 (1995) 98-113.
35. Piezo Systems, Inc., 186 Massachussets Avenue, Cambridge, MA.
36. G. Surace, V. Anghel, C. Mores, Coupled bending-torsion vibration analysis of rotating pretwisted blades: an integral formulation and numerical examples, Journal of Sound and Vibration 206 (1997) 473-486.
37. O. Song, N. Jeong, Vibration and stability of pretwisted spinning thin-walled composite beams featuring bending-elastic coupling, Journal of Sound and Vibration 237 (2000) 513-533.
38. H. Yoo, J. Kwak, J. Chung, Vibration analysis of rotating pre-twisted blades with a concentrated tip mass, Journal of Sound and Vibration 270 (2001) 839-853.