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Flutter control using resistively shunted piezoceramics

Published online by Cambridge University Press:  03 February 2016

S. B. Kandagal  and
K. Venkatraman
S. B. Kandagal
Affiliation:
[email protected], Department of Aerospace Engineering, Indian Institute of Science Bangalore, India
K. Venkatraman
Affiliation:
[email protected], Department of Aerospace Engineering, Indian Institute of Science Bangalore, India
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Abstract

This paper investigates the feasibility of flutter control using resistively shunted piezoceramics. 2D aerofoil model is elastically restrained in heave and pitch by a set of leaf springs modeled as Bernoulli-Euler beams. The piezoceramic transducers are bonded to the leaf springs. Unsteady aerodynamic theory is used to solve the flutter determinant incorporating the additive damping terms due to resistive shunting. Tuned dampers realised by resistive shunted piezoceramics in heave and pitch springs could enhance flutter speed in the range 25-50 % based on additive damping of 10 % achieved due to resistive shunting of piezoceramics in either pitch spring, heave spring or both.

Type
Research Article
Information
The Aeronautical Journal , Volume 114 , Issue 1156 , June 2010 , pp. 387 - 390
Copyright
Copyright © Royal Aeronautical Society 2010 

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References

1. Crawley, E.F., Intelligent structures for aerospace: A technology overview and assessment, AIAA J, 1994, 32, (8), pp 1689–1699.Google Scholar
2. Horikawa, H. and Dowell, E.H., An elementary explanation of the flutter mechanism with active feedback controls, J Aircr, 1979, 16, (4), pp 225–232.Google Scholar
3. Lazarus, K.B, Crawley, E.F. and Lin, C.Y., Fundamental mechanics of aeroelastic control with control surface and strain actuation, J Guidance, Control and Dynamics, 1995, 18, (1), pp 10–17.Google Scholar
4. Nitzsche, F., Liberatore, S. and Zimcik, , Theoretical and experimental investigations on an active control system for vertical fin buffeting alleviation using strain actuation, Aeronaut J, 2001, 105, (1047), pp 277–285.Google Scholar
5. Abramovich, H, Weller, T. and Ping, S.Y., Dynamic Response of a high aspect ratio wing equipped with PZT patches — A theoretical and experimental study, J Int Mat Systems and Structures, 2005, 16, pp 919–923.Google Scholar
6. Tuzscu, I. and Meirovitch, L., Control of flying flexible aircraft using control surfaces and dispersed piezoelectric actuators, Smart Materials and Structures, 2006, 15, pp 893–903.Google Scholar
7. Chopra, I., Review of the state of the art of smart structures and integrated systems, AIAA J, 2002, 40, (11), pp 2145–2187.Google Scholar
8. Hurlebaus, S. and Gaul, L., Smart structure dynamics, Mech Systems and Signal Processing, 2006, 20, pp 255–281.Google Scholar
9. Hagood, N.W. and Flotow, A. Von. Damping of structural vibrations with piezoelectric materials and passive electrical networks, J Sound Vib, 1991, 146, (2), pp 243–268.Google Scholar
10. Moheimani, S.O., A survey of recent innovations in vibration damping and control using shunted piezoelectric transducer, IEEE Trans on Control Systems Technology, 2003, 11, pp 482–494.Google Scholar
11. Shu, Y.C. and Lien, I.C., Analysis of power output for piezoelectric energy harvesting systems, Smart Materials and Structures, 2006, 15, pp 1499–1512.Google Scholar
12. Tang, J. and Wang, K.W., Active and Passive hybrid piezoelectric networks for vibration control comparison and improvement, Smart Materials and Structures, 2001, 10, pp 794–806.Google Scholar
13. Agneni, A., Mastroddi, F. and Polli, G.M., Shunted piezoelectric patches in elastic and aeroelastic vibrations, Computers and Structures, 2003, 81, pp 91–105.Google Scholar
14. Kandagal, S.B. and Venkatraman, K., Closed-loop flutter control using strain actuation, Aeronaut J, 2004, 108, (1083), pp 271–275.Google Scholar
15. Niederberger, D. and Morari, M., An autonomous shunt circuit for vibration damping, Smart Materials and Structures, 2006, 15, pp 359–364.Google Scholar
16. Kandagal, S.B. and Venkatraman, K., Form factors for vibration control of beams using resistively shunted piezoceramics, J Sound Vib 2004, 274, pp 1123–1133.Google Scholar
17. Bisplinghoff, R.L., Ashley, H. and Halfman, R.L., Aeroelasticity, 1955, Addison-Wesley Publishing, Cambridge, UK.Google Scholar