Feasibility analysis of using piezoceramic transducers for cantilever beam modal testing
Source abstract
Abstract
This paper presents a theoretical analysis of the application of piezoceramic transducers to cantilever beam modal testing. Four pairs of sensors and actuators, including accelerometer - point force, accelerometer - PZT, PVDF - point force and PVDF - PZT, are considered. The frequency response functions (FRFs) for the four pairs of sensors and actuators are first derived and written in the conventional modal format. The characteristics of modal parameters can thus be interpreted through the FRFs. A column of the FRF matrix can then be obtained based on the theoretical formulation. A curve-fitting algorithm is then applied to extract the modal parameters, such as natural frequencies, mode shapes and damping ratios. Results show that any sensor - actuator pair can successfully determine natural frequencies and damping ratios. Point types of transducer result in the displacement mode shapes, while piezoceramic transducers that are strip types and distributed in sense give the mode shapes of the slope difference between the edges of piezoceramic transducers. The paper provides the theoretical basis of applying piezoceramic transducers to experimental modal analysis and numerically supports the feasibility of cantilever beam modal testing using piezoceramic transducers.
Source: openalex_inverted_index · Quality: baseline
Research context
OpenAlex topics: Structural Health Monitoring Techniques · Aeroelasticity and Vibration Control · Ultrasonics and Acoustic Wave Propagation
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (32)
Show source-provided references
1. Han S · Int. J. Anal. Exp. Modal Anal. · 1991 · 6 · 147
2. Ebersbach P · Int. J. Anal. Exp. Modal Anal. · 1989 · 4 · 109
3. El-Deeb K M M · Int. J. Anal. Exp. Modal Anal. · 1992 · 7 · 51
4. Song S H · Int. J. Anal. Exp. Modal Anal. · 1993 · 8 · 263
5. Worden K · Int. J. Anal. Exp. Modal Anal. · 1994 · 9 · 35
6. Wright J R · Int. J. Anal. Exp. Modal Anal. · 1991 · 6 · 89
7. Sriram P · Int. J. Anal. Exp. Modal Anal. · 1990 · 5 · 155
8. Zhang P Q · Int. J. Anal. Exp. Modal Anal. · 1992 · 7 · 243
9. Collins S A · J. Guidance Control · 1992 · 15 · 39610.2514/3.20849 ↗
10. Clark R L · J. Acoust. Soc. Am. · 1992 · 91 · 332110.1121/1.402822 ↗
11. Wang B T · Smart Mater. Struct. · 1994 · 3 · 47610.1088/0964-1726/3/4/010 ↗
12. Young A J · J. Intell. Mater. Syst. Struct. · 1994 · 5 · 53610.1177/1045389X9400500410 ↗
13. Crawley E F · AIAA J. · 1987 · 25 · 137310.2514/3.9792 ↗
14. Clark R L · J. Acoust. Soc. Am. · 1991 · 90 · 34610.1121/1.401257 ↗
15. Wang B T · J. Composite Mater. · 1991 · 25 · 43310.1177/002199839102500405 ↗
16. Wang B T · J. Intell. Mater. Syst. Struct. · 1991 · 2 · 3810.1177/1045389X9100200103 ↗
17. Gibbs G P · J. Acoust. Soc. Am. · 1992 · 92 · 322110.1121/1.404172 ↗
18. Charette F · J. Acoust. Soc. Am. · 1994 · 96 · 227210.1121/1.410099 ↗
19. Bailey T · J. Guidance Control · 1986 · 6 · 605
20. Clark R L · J. Intell. Mater. Syst. Struct. · 1993 · 4 · 35410.1177/1045389X9300400308 ↗
21. Im S · AIAA J. · 1989 · 27 · 180110.2514/3.10337 ↗
22. Dimitriadis E K · J. Vib. Acoust. · 1991 · 113 · 10010.1115/1.2930143 ↗
23. Lester H C · J. Intell. Mater. Syst. Struct. · 1993 · 4 · 29510.1177/1045389X9300400302 ↗
24. Sun F P · 1994 · 871
25. Cole D G · 1994 · 521
26. Meirovitch L · 1986
27. Hubbard J E · 1987 · 407
28. Wang B T · 1995 · 805
29. LMS · 1993
30. Piezo Systems · 1990
31. Pennwalt Corporation · 1990
32. Wang B T · J. Technol.