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Identification of noise generation and flow kinematics in the air gap for two different blade tip designs of an axial fan

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Abstract

Importance of the role of axial fans in our everyday life as well as in industrial sphere is crucial. Their presence dictates indispensable reduction of the emitted noise level. The aerodynamically born noise due to the kinematics of the air-flow in the gap between rotor and stator is one predominant source of emitted noise by most fans and is the most intensive within the human audible spectrum. Two different rotor blade tip shapes A and B were analysed in details and the results presented in this paper. Their influence on the emitted noise was determined by measurements of the integral aerodynamic characteristic and by the level of the sound pressure level of the fan. It was confirmed that the kinematics of the air-flow within the blade tip gap is significantly different for both observed blade tip designs and plays a crucial role when generation and size of the total emitted noise power is concerned. Frequency spectra of the measured noise pressure level for both observed blade designs was also essentially different and served to confirm the well-known fact that intensity of the sound pressure level decreases with the frequency, which helps to assess and identify mechanisms of the noise generation. A typical measured amplitude decrease of the sound pressure level was observed and explained in details for both blade tip versions for the frequency range f>1000 Hz: appropriate scaling for the blade tip A and for the blade tip B was determined as \(\omega^{-2.8}\) and \(\omega^{-4/3}\) respectively. Distinctive differences between the two observed frequency spectra were established. Identification of locations, sources and specificity of the generated noise together with their detailed explanation was made possible by measurements of local pressure, velocity and their variances and is supported by simultaneous experimental flow visualization.

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Literatur

  1. Rains DA (1954) Tip clearance flows in axial flow compressors and pumps. California institute of technology, Hydrodynamics and mechanical engineering laboratories, Report No. 5, California

  2. Varva MH (1960) Aerothermodynamics and flow in turbomachines. John Wiley & Sons, New York

  3. Senoo Y, Ishida M (1986) Pressure loss due to the tip clearance of impeller blades in centrifugal and axial blowers. J Eng Gas Turbines Power 108:32–37

  4. Lakshminarayana B, Horlock JH (1962) Tip-clearance flow and losses for an isolated compressor blade. British ARC R& M 3316

  5. Gusakova EA, Mikhailova VA, Tyryshkin VG (1960) Features of the flow over the end parts of nonshrouded blades and their influence on the efficiency of a turbine stage. Teploenergetika 17:4

  6. Mehmel D (1962) Clearance flow in cascades. Ing Arch 31:294

  7. Inoue M, Kuroumaru M, Fukuhara M (1986) Behavior of tip leakage flow behind an axial compressor rotor. J Eng Power 108(1):7–14

  8. Longhouse RE (1978) Control of tip-vortex noise of axial flow fans by rotating shrouds. J Sound Vib 58:201–214

  9. Fukano T, Takamatsu Y, Kodama Y (1986) The effects of tip clearance on the noise of low pressure axial and mixed flow fans. J Sound Vib 105:291–308

  10. Kameier F, Neise W (1997) Experimental study of tip clearance losses and noise in axial turbomachines and their reduction. J Turbomach 119:460–471

  11. Milavec M, Širok B, Vidal D, Hočevar M (2014) Influence of the shape of the blade tip on the emitted noise in the air-gap between the rotor and the housing of an axial fan. Forsch Ingenieurwes 78(3–4): 107 -119

  12. Corsini A, Sheard AG (2007) Tip end-plate concept based on leakage vortex rotation number control. J Comput Appl Mech 8:21–37

  13. Corsini A, Rispoli F, Sheard AG (2007) Development of improved blade tip end plate concepts for low-noise operation in industrial fans. J Power Energ 221:669–681

  14. Biannchi S, Corsini A, Rispoli F, Sheard AG (2009) Experimental development of a measurement technique to resolve the radial distribution of a fan aero-acoustic emissions. Noise Control Eng J 57:360–369

  15. Kolmogorov AN (1941) Dissipation of energy in the locally isotropic turbulence. Proceedings of the USSR Academy of Sciences 32:16–18

  16. Nore C, Abid M, Brachet ME (1997) Decaying Kolmogorov turbulence in a model of super flow. Phys Fluids 9(9):2644 -267

  17. Adzhemyan TL, Hnatich M, Horvath D, Stehlik M (1998) Calculation of spectra of turbulence in the energy-containing and inertial ranges. Phys Rev E 58:4511

  18. Xia H, Francois N, Punzmann H, Shats M (2013) Lagrangian scale of particle dispersion in turbulence. Nat Commun 4

  19. Rubinstein R, Zhou Y (1997) Time correlations and the frequency spectrum of sound radiated by turbulent flows. Institute for Computer Applications in Science and Engineering NASA Langley Research Center Hampton, NASA Contractor Report No. 201648

  20. Alič G, Širok B, Hočevar M (2010) Method for modifying axial fan’s guard grill and its impact on operating characteristics. Forsch Ingenieurwes 74:87–98

  21. Holeček N, Širok B, Hočevar M, Podgornik R, Grudnik R (2006) Reducing the noise emitted from a domestic clothes-drying machine. Noise Control Eng J 54(3):137–145

  22. Tam CKW, Golebiowski M, Seiner JM (1996) On the two components of turbulent mixing noise from supersonic jets, 2nd AIAA/CEAS Aeroacoustics Conference, State College, PA, 1716 -1729

  23. International organization for standardization ISO 5801: Industrial fans; Performance testing using standardizied airways (2009)

  24. International organization for standardization ISO 3741: Acoustics; determination of sound powerlevels of noise sources using sound pressure - precision methods for reverberation rooms (2010)

  25. International organization for standardization ISO 13347-1/2: Industrial fans; Determination of fan sound power levels under standardized laboratory conditions - reverberant room method (2004)

  26. Lakshminarayana B (1996) Fluid dynamics and heat transfer of turbomachinery. John Wiley & Sons, New York

  27. Papamoschou D, Roshko A (1998) The compressible turbulent shear layers: an experimental study. Fluid Mech 197:453–477

  28. Bogdanof DW (1988) Compressible effects in turbulent shear layers. AIAA J 21:926–927

  29. Sturm H, Dumstorff G, Busche P, Westermann D, Lang W (2012) Boundary layer separation and reattachment detection on airfoils by thermal flow sensors. Sensors 12:14292–14306

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Milavec, M., Širok, B., Vidal de Ventos, D. et al. Identification of noise generation and flow kinematics in the air gap for two different blade tip designs of an axial fan. Forsch Ingenieurwes 79, 29–39 (2015). https://doi.org/10.1007/s10010-015-0185-2

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  • DOI: https://doi.org/10.1007/s10010-015-0185-2

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