Preview

Acoustic Vibrations in Gas Pipelines

Powerful Essays
Open Document
Open Document
11931 Words
Grammar
Grammar
Plagiarism
Plagiarism
Writing
Writing
Score
Score
Acoustic Vibrations in Gas Pipelines
Journal of Sound and Vibration (1995) 184(2), 343–368

HIGH AMPLITUDE VORTEX-INDUCED PULSATIONS IN A GAS TRANSPORT SYSTEM
P. C. K, M. C. A. M. P, A. H  A. P. J. W
Eindhoven University of Technology, W & S 1.53, P.O. Box 513, Eindhoven, The Netherlands

A. I, G. R  R. P
University ‘La Sapienza’, Via Eudossiana 18, 00184 Rome, Italy

 J. C. B
TPD/TNO, P.O. Box 155, 2600 AD Delft, The Netherlands (Received 17 January 1994, and in final form 7 June 1994) High Reynolds number, low Mach number gas flows in pipe systems with closed side branches exhibit spectacular low frequency self-sustained pulsations driven by periodic vortex shedding at specific values of the Strouhal number. A detailed study is presented of the behaviour of the flow in a system with two opposite closed side branches of equal length in a cross configuration. For junctions with both sharp and rounded edges the acoustic flow velocity amplitude is comparable to the main flow velocity. A two-dimensional potential flow model based on the vortex blob method, used to simulate the flow in the junction, describes accurately the flow visualization and laser Doppler data obtained in pipes with square cross-sections and with sharp edged junctions. The numerical simulation is used to calculate the acoustical power generated by the vortical flow at a given amplitude of the acoustic velocity field and Strouhal number. In reality, for a pulsation with constant amplitude, this power is balanced by the viscothermal losses and acoustic radiation, which is the basis for the indirect measurement of the source power. It is shown that, for the acoustic amplitude observed, radiation losses due to the generation of non-resonating harmonics by wavesteepening has to be taken into account in the energy balance. This finding is confirmed by the appearance of shock waves in the geometry with rounded edges.
7 1995 Academic Press Limited

1. INTRODUCTION

The present



References: 1. J. C. B, A. P. J. W and J. G 1986 AIAA 10th Aeroacoustics Conference, Seattle, Washington, 9–11 July, AIAA paper 86-192. Self sustained low frequency resonance in low Mach number gas flow through pipelines with side branch cavities. 2. J. C. B 1987 Ph.D. Thesis, Eindhoven University of Technology. Flow induced pulsations in pipe systems. 3. J. C. B, A. H, M. E. H.  D, A. P. J. W and J. G 1989 Journal of Fluids Engineering 111, 484–491. Flow induced pulsations in gas transport systems: analysis of the influence of closed side branches. 4. J. C. B, A. H, M. E. H.  D, A. P. J. W and J. G 1991 Journal of Sound and Vibration 150, 371–393. Self-sustained aero-acoustic pulsations in gas transport systems: experimental study of the influence of closed side branches. 5. Y. N. C 1980 In Proceedings of the Symposium on Practical Experience with Flow-induced Vibrations, (E. Naudascher and D. Rockwell, editors), 265–279. Berlin: Springer-Verlag. Experiences with flow-induced vibrations at sulzer. 6. S. Z and E. T. B¨ 1992 Journal of Fluids and Structures 6, 583–601. Self-excited resonances of two side-branches in close proximity. 7. W. M. J, K. K. B and W. S 1989 Journal of Sound and Vibration 131, 265–285. Cylindrical side-branch as tone generator. 8. W. M. J and W. S 1989 U.S. Patent No. 486 71 90: Damping pressure pulsations in piping systems. 9. A. J. C and P. S. B 1973 Journal of Computational Physics 13, 423–429. Discretisation of a vortex sheet, with an example of roll-up. 10. R. K 1987 Journal of Fluid Mechanics 184, 123–155. Computation of vortex sheet roll-up on the Trefftz plane. 11. M. C. A. M. P 1993 Ph.D. Thesis, Eindhoven University of Technology. Aeroacoustic sources in internal flows. 12. M. S. H 1975 Journal of Fluid Mechanics 71(4), 625–673. Contributions to the theory of aerodynamic sound with applications to excess jet noise and the theory of the flute. 368 . .   . 13. M. S. H 1984 Journal of Applied Mathematics 32, 187–209. On the absorption of sound by turbulence and other hydrodynamic flows. 14. A. P 1964 Journal of the Acoustical Society of America 36(1), 177–195. Theory of vortex sound. 15. D. R and E. N 1978 Journal of Fluids Engineering 100, 152–165. Review. Self-sustained oscillations of flow past cavities. 16. D. R 1983 American Institute of Aeronautics and Astronautics Journal 21(5), 645–664. Oscillations of impinging shear layers. 17. W. K. B and A. P 1983 Proceedings of the Conference on Recent Advances in Aeroacoustics, 249–325. The development of contemporary views of flow-tone generation. 18. R. D. B 1984 Journal of Sound and Vibration 92, 455–470. Review of sound induced by vortex shedding from cylinders. 19. S. A. E Journal of the Acoustical Society of America 67(3), 774–781. Forced oscillations of a separated shear layer with application to cavity flow-tone effects. 20. M. S. H 1980 Journal of Sound and Vibration 70, 407–411. The dissipation of sound at an edge. 21. P. A. N, N. H and P. E. D 1983 Journal of Sound and Vibration 91, 375–402. Fluid dynamics of a flow excited resonance, part II: flow acoustic interaction. The dissipation of sound at an edge. 22. A. N. S and M. C. W 1986 Journal of Sound and Vibration 104, 55–73. Flow-resonant sound interaction in a duct containing a plate, II: square leading edge. 23. M. K. M 1986 Journal of Sound and Vibration 109, 277–284. An exact energy corollary for homentropic flow. 24. P. L. J 1989 Journal of Sound and Vibration 131, 37–66. The sound power from turbulence: a theory of the exchange of energy between the acoustic and non-acoustic fields. 25. P. E. D 1989 Journal of Sound and Vibration 131, 67–90. Momentum potential theory of energy flux carried by momentum fluctuations. 26. P. E. D 1993 Acoustics ‘93, Proceedings of the Institute of Acoustics, Spring Meeting, Southampton (April 1993) 15(3), 891–900. Sources of radiated acoustical waves in fluids. 27. R. K 1986 Journal of Fluid Mechanics 167, 65–93. A study of singularity formation in a vortex sheet by the point vortex method. 28. J. H. M. D and L.  W 1980 Journal of Fluid Mechanics 99, 293–319. Flow in the exit of open pipes during acoustic resonance. 29. A. D. P 1989 Acoustics, an Introduction to its Physical Principles and Applications. New York: McGraw-Hill. 30. O. V. R and S. I. S 1977 Theoretical Foundations of Nonlinear Acoustics. Studies in Soviet Science.

You May Also Find These Documents Helpful

  • Good Essays

    Nt1310 Unit 3 Lab Report

    • 3999 Words
    • 16 Pages

    This solution is then used as initial value for the transient simulation. In the unsteady simulations, the motion of the center blade was prescribed by a set of equations for the requested mode. The correctness of the imposed motion is confirmed by an analytical model. A timemarching solution was acquired spanning typically 3 oscillation periods. The flow could be regarded as time periodic already after the second oscillation cycle (criterion used: >0.5% phase-locked difference). A time trace of unsteady pressure coefficient at a chosen point on the blade surface is presented in Figure 6.3. One oscillation period was resolved by 20 time steps and with three iteration loops per time…

    • 3999 Words
    • 16 Pages
    Good Essays
  • Better Essays

    [2] Queen Mary University of London, DEN233, Low Speed Aerodynamics, Lecture Notes, 2013, (Accessed on 13th November 2013)…

    • 2962 Words
    • 12 Pages
    Better Essays
  • Better Essays

    Waves Lab

    • 1296 Words
    • 6 Pages

    The purpose of this laboratory experiment is to “investigate how the vibrating source affects selected characteristics of the sound produced” (Giancoli, 2006).…

    • 1296 Words
    • 6 Pages
    Better Essays
  • Good Essays

    Physics Mastery Lab

    • 836 Words
    • 4 Pages

    The purpose of this experiment is to measure the speed of sound in air and to determine the effects of frequency on the speed of sound.…

    • 836 Words
    • 4 Pages
    Good Essays
  • Better Essays

    As a result of the experiment and computation of data, the aerofoil was found to have a critical Mach number of M=0.732. Below this freestream Mach number the Prandtl-Glauert law predicted results very successfully. However, above this value, the law completely breaks down. This was found to be the result of local regions of supersonic flow and local shockwaves.…

    • 2069 Words
    • 9 Pages
    Better Essays
  • Good Essays

    Sound In Air Lab

    • 964 Words
    • 4 Pages

    Sound is a longitudinal (compressional) wave caused by a vibrating source. In this experiment, we use standing sound waves created by the tuning forks to determine the speed of sound in air in a tube when it reaches different resonances. In this lab we focused primarily on using standing sound waves (compressional waves) created by tuning forks in order to determine the speed of sound in air in a tube when it reaches resonance.…

    • 964 Words
    • 4 Pages
    Good Essays
  • Powerful Essays

    clarinet or organ pipe can be modeled using the one-dimensional wave by substituting airpressure deviation for string displacement, and longitudinal volume velocity for transverse…

    • 1680 Words
    • 7 Pages
    Powerful Essays
  • Powerful Essays

    Hedrick, W. R., & Hykes, D. L., 2005. Ultrasound physics and instrumentation (4th ed.). St. Louis, Mo.: Elsevier Mosby.…

    • 1185 Words
    • 5 Pages
    Powerful Essays
  • Good Essays

    Tuning Forks Lab Report

    • 474 Words
    • 2 Pages

    The objective of this lab was to investigate the resonances of tuning forks with various natural vibrating frequency. The student would also evaluate the speed of sound in air with the resonances. There…

    • 474 Words
    • 2 Pages
    Good Essays
  • Good Essays

    Acoustic Guitar Essay

    • 461 Words
    • 2 Pages

    Perhaps the most overlooked mechanics in the physics of guitars is the effect of air cavity on the sound. And whilst the strings, face plates and black plates all have distinctive modes which help uncover their individual tones, so does the air in a guitar. Needless to say, it is from this air cavity that the Helmholtz Resonance is able to thrive- the lowest frequency of air resonance is customarily reliant on the volume of air, and the shape and sound of a guitar’s sound hole. Given this foundation…

    • 461 Words
    • 2 Pages
    Good Essays
  • Satisfactory Essays

    In conclusion the hydrodynamic cavitation reactors provide huge potential and convincing approach for various immediate industrial scale implementations as compared to acoustic reactors. Moreover, the feasibility of scale up of this reactor is relatively easier since plenty of research has already been done on fluid dynamics in the downstream of constriction valves. The operating efficiency and energy dissipation also goes down we scale up the reactor.…

    • 67 Words
    • 1 Page
    Satisfactory Essays
  • Best Essays

    Organ Pipes, Acoustics. 2012. Organ Pipes, Acoustics. [ONLINE] Available at: http://www2.ibp.fraunhofer.de/akustik/ma/pipesound/index_e.html. [Accessed 10 May 2012].…

    • 798 Words
    • 4 Pages
    Best Essays
  • Good Essays

    Ultrasound

    • 2365 Words
    • 10 Pages

    2- Acoustic streaming ( it is the unidirectional movement of the fluid in the US field which leads to:…

    • 2365 Words
    • 10 Pages
    Good Essays
  • Good Essays

    Sound Wave

    • 564 Words
    • 3 Pages

    Resonance can be observed on a tube with one end open. Musical tones can be…

    • 564 Words
    • 3 Pages
    Good Essays
  • Powerful Essays

    Resonance Tube Lab

    • 1242 Words
    • 5 Pages

    Resonance 1 Williams Lab 1: Tube Staci Williams Kevin Schesing, Nicole Harty, Caitlin Kubota Section 015 2 Performed February 2, 2010 Due February 13, 2010 3 Theory: 2.1 Air As A Spring Williams Gas is a springy material, and when placed in a cylinder with pistons on each side it can be compressed as pistons push in, raising the pressure inside. There will be a net force from the pressure to push the piston back out. Since gas has mass it can support oscillations and waves. 2.2 Traveling Sound Waves in Air When a cone of a speaker moves out, it compresses air next to is and imparts an outward velocity to the air molecules around it, in addition to the random thermal velocities of air molecules. The molecules nearest to the speaker will collide with those near them and impart those molecules into motion, propagating away from the speaker producing sound. Similar statements apply to when the cone is moved in as well. If speaker cone vibrates sinusoidally, a traveling wave will be emitted form the speaker and the wave relation f = v < = wavelength, f = frequency of wave, v = velocity of wave> is satisfied. AS the motion of the wave molecules move along the direction of the propagation of the wave are called longitudinal waves, which is contrasting to transverse waves which are on strings. The waves as the elements of the string move transverse to the direction in which the waves travel. In traveling waves the displacement of air satisfies the wave equation. V = (P/) < v = velocity of wave, = specific heats at constant pressure/ " constant volume = Cp/Cv, P = air pressure, = air mass density>. With the ideal gas law it can be written as V = (RT/M ) < R = molar gas constant, T = absolute temperature, M = Molar mass>. For a given gas the speed will be proportional to the square root of the temperature giving the equation vrms = (3RT/M) < vrms ~ thermal speed of the gas molecules>. The speed of sound in gas is close to the thermal speed of molecules in gas, so the…

    • 1242 Words
    • 5 Pages
    Powerful Essays