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Research Papers: Fluid-Structure Interaction

Flow-Excited Acoustic Resonance of Isolated Cylinders in Cross-Flow

[+] Author and Article Information
Nadim Arafa

AeroAcoustics and Noise Control Laboratory,
University of Ontario Institute of Technology,
2000 Simcoe Street North,
Oshawa, ON L1H7K4, Canada
e-mail: nadim.arafa@uoit.ca

Atef Mohany

AeroAcoustics and Noise Control Laboratory,
University of Ontario Institute of Technology,
2000 Simcoe Street North,
Oshawa, ON L1H7K4, Canada
e-mail: atef.mohany@uoit.ca

1Corresponding author.

Contributed by the Pressure Vessel and Piping Division of ASME for publication in the JOURNAL OF PRESSURE VESSEL TECHNOLOGY. Manuscript received December 1, 2014; final manuscript received March 23, 2015; published online August 25, 2015. Assoc. Editor: Jong Chull Jo.

J. Pressure Vessel Technol 138(1), 011302 (Aug 25, 2015) (8 pages) Paper No: PVT-14-1195; doi: 10.1115/1.4030270 History: Received December 01, 2014

The flow-excited acoustic resonance of isolated cylinders in cross-flow is investigated experimentally where the effect of the cylinder(s) proximity to the acoustic particle velocity nodes of the cross-modes is presented in this paper. For the case of a single cylinder, the cylinder's location does not significantly affect the vortex shedding process; however, it affects the excitation level of each acoustic cross-mode. When the cylinder is moved away from the acoustic particle velocity antinode of a specific acoustic cross-mode, a combination of the cross-modes is excited with intensities that seem to be proportional to the ratio of the acoustic particle velocities of these modes at the cylinder's location. For the cases of two and three hydrodynamically uncoupled cylinders positioned simultaneously side-by-side in the duct, it is observed that the first three acoustic cross-modes are excited. When one cylinder is positioned at the acoustic particle velocity antinode of a specific cross-mode and another cylinder is positioned at its acoustic particle velocity node, i.e., a cylinder that should excite the resonance and another one that should not excite it, respectively; the excitation always takes over and the resonance occurs at a further elevated levels. It is also observed that the acoustic pressure levels in the cases of multiple cylinders are not resulting from a linear superposition of the excited level obtained from each individual cylinder which indicates that the removal of cylinders at certain locations may not be a viable technique to eliminate the acoustic resonance in the case of tube bundles.

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References

Blevins, R. D. , and Bressler, M. M. , 1987, “Acoustic Resonance in Heat Exchanger Tube Bundles—Part I: Physical Nature of the Phenomenon,” ASME J. Pressure Vessel Technol., 109(3), pp. 275–281. [CrossRef]
Ziada, S. , Oengoren, A. , and Buhlmann, E. T. , 1989, “On Acoustical Resonance in Tube Arrays: Part I. Experiments,” J. Fluids Struct., 3(3), pp. 293–314. [CrossRef]
Ziada, S. , and Oengoren, A. , 1990, “Flow-Induced Acoustical Resonance of In-Line Tube Bundles,” Sulzer Technical Review, Vol. 1, Sulzer Management AG, Sulzer Technical Review, Winterthur, pp. 45–47.
Ziada, S. , and Oengoren, A. , 1992, “Vorticity Shedding and Acoustic Resonance in an In-Line Tube Bundle Part I: Vorticity shedding,” J. Fluids Struct., 6(3), pp. 271–292. [CrossRef]
Oengoren, A. , and Ziada, S. , 1992, “Vorticity Shedding and Acoustic Resonance in an In-Line Tube Bundle Part II: Acoustic Resonance,” J. Fluids Struct., 6(3), pp. 293–302. [CrossRef]
Blevins, R. D. , and Bressler, M. M. , 1993, “Experiments on Acoustic Resonance in Heat Exchanger Tube Bundles,” J. Sound Vib., 164(3), pp. 503–533. [CrossRef]
Eisinger, F. L. , Francis, J. T. , and Sullivan, R. E. , 1996, “Prediction of Acoustic Vibration in Steam Generator and Heat Exchanger Tube Banks,” ASME J. Pressure Vessel Technol., 118(2), pp. 221–236. [CrossRef]
Eisinger, F. L. , and Sullivan, R. E. , 2003, “Suppression of Acoustic Waves in Steam Generator and Heat Exchanger Tube Banks,” ASME J. Pressure Vessel Technol., 125(2), pp. 221–227. [CrossRef]
Feenstra, P. A. , Weaver, D. S. , and Eisinger, F. L. , 2006, “A Study of Acoustic Resonance in a Staggered Tube Array,” ASME J. Pressure Vessel Technol., 128(4), pp. 533–540. [CrossRef]
Ziada, S. , and Lafon, P. , 2014, “Flow-Excited Acoustic Resonance Excitation Mechanism, Design Guidelines, and Counter Measures,” ASME J. Appl. Mech. Rev., 66(1), p. 011002. [CrossRef]
Mohany, A. , and Ziada, S. , 2005, “Flow-Excited Acoustic Resonance of Two Tandem Cylinders in Cross-Flow,” J. Fluids Struct., 21(1), pp. 103–119. [CrossRef]
Mohany, A. , 2006, “Flow–Sound Interaction Mechanisms of a Single and Two Tandem Cylinders in Cross-Flow,” Ph.D. thesis, McMaster University, Hamilton.
Hanson, R. , Mohany, A. , and Ziada, S. , 2009, “Flow-Excited Acoustic Resonance of Two Side-By Side Cylinders in Cross-Flow,” J. Fluids Struct., 25(1), pp. 80–94. [CrossRef]
Mohany, A. , and Ziada, S. , 2009, “A Parametric Study of the Resonance Mechanism of Two Tandem Cylinders in Cross-Flow,” ASME J. Pressure Vessel Technol., 131(2), p. 021302. [CrossRef]
Mohany, A. , and Ziada, S. , 2009, “Effect of Acoustic Resonance on the Dynamic Lift Forces Acting on Two Tandem Cylinders in Cross-Flow,” J. Fluids Struct., 25(3), pp. 461–478. [CrossRef]
Mohany, A. , and Ziada, S. , 2011, “Measurements of the Dynamic Lift Force Acting on a Circular Cylinder in Cross-Flow and Exposed to Acoustic Resonance,” J. Fluids Struct., 27(8), pp. 1149–1164. [CrossRef]
Mohany, A. , Arthurs, D. , Bolduc, M. , Hassan, M. , and Ziada, S. , 2014, “Numerical and Experimental Investigations of Flow-Acoustic Resonance of Side-By-Side Cylinders in a Duct,” J. Fluids Struct., 48, pp. 316–331. [CrossRef]
Sumner, D. , 2010, “Two Circular Cylinders in Cross-Flow: A Review,” J. Fluids Struct., 26(6), pp. 849–899. [CrossRef]
Blevins, R. D. , and Bressler, M. M. , 1987, “Acoustic Resonance in Heat Exchanger Tube Bundles—Part II: Prediction and Suppression of Resonance,” ASME J. Pressure Vessel Technol., 109(3), pp. 282–288. [CrossRef]
Walker, E. M. , and Reising, G. F. S. , 1968, “Flow-Induced Vibrations in Cross-Flow Heat Exchangers,” Chem. Process Eng., 49, pp. 95–103.
Zdravkovich, M. M. , and Nuttall, J. A. , 1974, “On the Elimination of Aerodynamic Noise in a Staggered Tube Bank,” J. Sound Vib., 34(2), pp. 173–177. [CrossRef]
Weaver, D. S. , 1993, “Vortex Shedding and Acoustic Resonance in Heat Exchanger Tube Arrays,” Technology for the '90s, M. K. Au-Yang, ed., ASME, New York, pp. 776–810.
Ziada, S. , and Oengoeren, A. , 1993, “Flow Structures in an In-Line Tube Bundle With Large Tube Spacings,” J. Fluids Struct., 7(6), pp. 661–687. [CrossRef]
Arafa, N. , Tariq, A. , Mohany, A. , and Hassan, M. , 2014, “Effect of Cylinder Location Inside a Rectangular Duct on the Excitation Mechanism of Acoustic Resonance,” J. Can. Acoust. Assoc., 42(1), pp. 33–40.
Kinsler, L. E. , Frey, A. R. , Coppens, A. B. , and Sanders, J. V. , 2000, Fundamentals of Acoustic, 4th ed., Wiley, New York.
Parker, R. , 1978, “Acoustic Resonances in Passages Containing Banks of Heat Exchanger Tubes,” J. Sound Vib., 57(2), pp. 245–260. [CrossRef]
Lienhard, J. H. , 1966, Synopsis of Lift, Drag, and Vortex Frequency Data for Rigid Circular Cylinder, Washington State University, College of Engineering, Research Division, Bulletin 300, Pullman.
Zdravkovich, M. M. , 1985, “Flow Induced Oscillations of Two Interfering Circular Cylinders,” J. Sound Vib., 101(4), pp. 511–521. [CrossRef]
Mohany, A. , and Ziada, S. , 2009, “Numerical Simulation of the Flow Sound Interaction Mechanisms of a Single and Two Tandem Cylinders in Cross-Flow,” ASME J. Pressure Vessel Technol., 131(3), p. 031306. [CrossRef]

Figures

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Fig. 1

Schematic of the experimental setup showing the acoustic particle velocity distribution along the duct height

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Fig. 2

Waterfall plot of the pressure spectra for a single cylinder positioned at Y/H = 0, D = 12.7 mm

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Fig. 3

Aeroacoustic response of a single cylinder in cross-flow positioned at Y/H = 0, D = 12.7 mm

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Fig. 4

Aeroacoustic response of a single cylinder in cross-flow positioned at Y/H = 0.25, D = 12.7 mm

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Fig. 5

Comparison of the aeroacoustic responses of a single cylinder positioned at two vertical locations, D = 12.7 mm

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Fig. 6

Comparison of the normalized acoustic pressure for a single cylinder positioned at various vertical locations, D = 12.7 mm

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Fig. 7

Distribution of the ratio of acoustic particle velocity to the maximum value of acoustic particle velocity for the first cross-mode. The theoretical normalized distribution of the acoustic particle velocity is shown in continuous line.

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Fig. 8

Comparison of the aeroacoustic responses of multiple cylinders, D = 12.7 mm. Cylinders are positioned at the acoustic particle velocity antinodes.

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Fig. 9

Comparison of the aeroacoustic responses of multiple cylinders, D = 12.7 mm. Cylinders are positioned at the acoustic particle velocity nodes.

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Fig. 10

Pressure drop versus the velocity for multiple cylinders, D = 12.7 mm

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Fig. 11

Contour plot of the normalized acoustic pressure distribution in the test section for the second cross-mode in the case of (a) empty duct, (b) single cylinder positioned at Y/H = 0, (c) single cylinder positioned at Y/H = 0.25, and (d) two cylinders positioned at Y/H = 0 and Y/H = 0.25

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Fig. 12

Normalized theoretical acoustic pressure distribution for the second acoustic cross-mode along the top wall of the test section versus the streamwise distance

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