University of Puget Sound Sound Ideas Summer Research Summer 2016 Vibrational Patterns in Curved Metal Plates Samuel D. Berling University of Puget Sound, [email protected] Follow this and additional works at: http://soundideas.pugetsound.edu/summer_research Part of the Other Physics Commons Recommended Citation Berling, Samuel D., "Vibrational Patterns in Curved Metal Plates" (2016). Summer Research. Paper 267. http://soundideas.pugetsound.edu/summer_research/267 This Article is brought to you for free and open access by Sound Ideas. It has been accepted for inclusion in Summer Research by an authorized administrator of Sound Ideas. For more information, please contact [email protected]. Vibrational Patterns in Curved Metal Plates Sam Berling Physics Department Summer 2016 Introduction Data The factors I investigated were (1) how plate size affected the frequency of a normal mode, (2) how The musical saw is an instrument played by using one hand to bend the saw into an s-shape and using the other hand to bow the saw. taper affects resonant frequency, (3) how curvature affected the confinement of a vibrational pattern to a localized region on a plate, and (4) whether the stress of a blade being bent affects the resonant frequency. I was particularly interested in the stress factor because one of the few papers on this topic assumes stress played no role in its analysis [1]. The musical saw inspired this more general study plates. I sought to identify factors affecting the vibrational patterns in curved metal plates. Plate Size To investigate how plate size affects the resonant frequencies of a given normal mode, I used three plates of two widths and two lengths [Figure 3]. I cut three plates to investigate taper, Plates 6, 7, and 8. Plates 6 and 8 were rectangular with Plate 6 being half the width of Plate 8. Plate 7 was tapered from the width of Plate 8 to the width of Plate 6 [Figure 4]. 3500 1400 1200 I used an Electronic Speckle-Pattern I the plates under certain conditions, and I used COMSOL Mutliphysics software [Figure 2] to Plate7 Plate8 2000 1500 Plate2 600 Plate1 horizontal nodal lines (called “(2, X)” modes) as plate length produces a much smaller increase in the resonant frequency of the frequency increases. 0 1 2 3 4 5 6 7 8 9 10 11 12 13 VerticalNodeNumber(X) Figure 4 A plot of resonant frequencies of (2, X) Modes for a tapered plate and two rectangular plates. • Figure 4 shows that the resonant frequencies of a tapered plate (Plate 7) are in between those of the 0 0 1 my method for finding resonant frequencies and normal modes. I focused on the modes with two roughly the same. are added, the difference in resonant 200 The ESPI combined with a spectrum analyzer was lines are added, the increase remains (2, 0) mode, but as vertical nodal lines 1000 Plate3 400 model the plates under those same conditions. 2500 Plate6 0 800 horizontal mode set but as vertical nodal • Figure 3 illustrates that a decrease in 500 1000 Frequency(Hz) Interferometry (ESPI) system [Figure 1] to image Frequency(Hz) Materials and Methods resonant frequencies of a given ResonantFrequenciesforPlates6,7,8for(2,X)Modes 3000 ResonantFrequenciesforPlates1,2,3for (2,X)Modes • Figure 3 illustrates that a decrease in plate width significantly increases the Taper on the vibrational patterns of curved metal Qualitative Results and Analysis 2 3 VerticalNodeNumber(X) corresponding wide (Plate 8) and narrow Curvature 4 Figure 3 A plot of resonant frequencies for (2, X) Modes. Plate 3 is the smallest, Plate 1 is the biggest, and Plate 2 is in between. these are generally the modes we hear when To study the effect of curvature, I clamped a rectangular plate (Plate 11) to create an s-shape, similar to those used in the playing of a musical saw, I then traced the shape and used a plot digitizer to import it into Excel [Figure 5]. • Figure 6 shows that the effect stress has on the resonant frequencies is negligible for curved plates with none differing by Plate11Shape1 playing an instrument such as the musical saw. (Plate 6) rectangular plates. 0.05 more than 5%. 0.04 Position(m) 0.03 Stress 0.01 • The curvature study showed that a 0 -0.01 0 0.05 0.1 0.15 0.2 0.25 0.3 0.35 0.4 0.45 -0.02 ResonantFrequenciesof(2,X)Modesfor Plates9,10 -0.04 plate. Figure 5 shows that the pattern Position(m) CurvatureofPlate11Shape1 occurs roughly where the curvature is less Plate9 Plate10 1 2 3 pattern occurs roughly at the inflection 1 0.5 point of the the double curve. 0 -0.5 0 0.1 0.2 0.3 0.4 -1 -1.5 -2 0 than 1 m-1 and that the center of the 1.5 Curvature(m-1) 1000 950 900 850 800 750 700 650 600 curved plate confines the vibrational patterns to a particular region on the -0.03 2 Frequency(Hz) Figure 1 ESPI Image of a plate vibrating at its (4,3) Mode. Mode numbers are denoted by the horizontal (4) and vertical (3) nodal lines, excluding the ends. White lines in ESPI images represent the nodal lines. To study the effect of stress, I compared the modes of a stressed curved plate (Plate 10) and an unstressed curved plate (Plate 9) [Figure 6]. 0.02 Position(m) 4 VerticalNodeNumber(X) References Figure 6 A comparison of resonant frequencies of (2, X) modes between a stressed plate (Plate 10) and an unstressed plate (Plate 9) of the same shape. [1] J. F. M. Scott; J. Woodhouse, “Vibration of an Elastic Strip with Varying Curvature” Philosophical Transaction: Physical Sciences and Engineering. Vol. 339, No. 1655 (1992): 587625. Figure 2 A COMSOL image representing the same (4,3) Mode as Figure 1. The blue lines in COMSOL images represent the nodal lines. Figure 5 The top is a digitized tracing of the shape Plate 11’s curve. The middle is a plot of the curvature of the shape. The bottom is an ESPI image of the plate resonating at the (2,0) mode. The green lines denote the edges of the plate. The orange lines denote the edges of the pattern of vibration. The red line denotes where the curvature is zero. Acknowledgments I would like to thank Professor Rand Worland for mentoring and advising me through this research process. I would also like to express my appreciation to the Washington NASA Space Grant Consortium for funding this research.
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