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Acoustics of a Mixed Porosity Felt Airfoil

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Advanced Research in Naval Engineering

Abstract

Lifting surfaces produce noise in operation, and porous materials have been shown to reduce this noise. Acoustic measurements were made on three arrangements of poroelastic material: full-chord impermeability, full-chord porosity, and “mixed” porosity. The results are compared to applicable published data. The noise reduction produced by the mixed porosity arrangement is found to be similar to the fully porous arrangement at low Reynolds numbers. The noise reduction produced by the mixed and fully porous foils shows significant differences at higher Reynolds numbers. A percolation-base physical model to explain elevated noise production at high frequencies is proposed.

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References

  1. T. Brooks, D. Pope, M. Marcolini, Airfoil self-noise and prediction, NASA, vol. 1218, 1989

    Google Scholar 

  2. R. Amiet, Noise due to turbulent flow past a trailing edge. J. Sound Vib. 47(3), 387–393 (1976)

    Article  Google Scholar 

  3. T. Bachmann, S. Klän, W. Baumgartner, M. Klaas, W. Schröder, H. Wagner, Morphometric characterisation of wing feathers of the barn owl Tyto alba pratincola and the pigeon Columba livia. Front. Zool. 4(1), 23 (2007)

    Article  Google Scholar 

  4. E. Sarradj, C. Fritzsche, T. Geyer, Silent owl flight: bird flyover noise measurements. AIAA J. 49(4), 769–779 (2011)

    Article  Google Scholar 

  5. T. Geyer, E. Sarradj, C. Fritzsche, Measurement of the noise generation at the trailing edge of porous airfoils. Exp. Fluids 48, 291–308 (2010)

    Article  Google Scholar 

  6. R. Hayden, R. Chanaud, Method of reducing sound generation in fluid flow systems embodying foil structures and the like. U.S. Patent 3,779,338, 1973

    Google Scholar 

  7. C. Ellett, Noiseless propeller. U.S. Patent 2,340,417, 1 Feb 1944

    Google Scholar 

  8. A. Gupta, T. Maeder, Wind-turbine blade and method for reducing noise in wind turbine. U.S. Patent 7,901,189, 2011

    Google Scholar 

  9. P. Ho, P. Gliebe, Low noise permeable airfoil. U.S. Patent 6,139,259, 2000

    Google Scholar 

  10. D. Kump, N. Lauziere, Method of controlling the permeability of a porous material, and turbine blade formed thereby. U.S. Patent 3,402,914, 24 Sept 1968

    Google Scholar 

  11. P. Hartwich, Porous airfoil and process. U.S. Patent 5,167,387, 1 Dec 1992

    Google Scholar 

  12. R. Mineck, P. Hartwich, Effect of full-chord porosity on aerodynamic characteristics of the NACA 0012 airfoil, NASA, 1996

    Google Scholar 

  13. J. Jaworski, N. Peake, Aerodynamic noise from a poroelastic edge with implications for the silent flight of owls. J. Fluid Mech. 723, 456–479 (2013)

    Article  MathSciNet  Google Scholar 

  14. M. Herr, K. S. Rossignol, J. Delfs, M. Mößner, N. Lippitz, Specification of porous materials for low-noise trailing-edge applications, in 20th AIAA/CEAS Aeroacoustics Conference, Atlanta, GA, Paper 3041-2014

    Google Scholar 

  15. M. Herr, A noise reduction study on flow-permeable trailing-edges, Deutsches Zentrum für Luft-und Raumfahrt, Institute of Aerodynamics and Flow Technology, Braunschweig, 2007

    Google Scholar 

  16. T. Brooks, T. Hodgson, Trailing edge noise prediction from measured surface pressures. J. Sound Vib. 78, 69–117 (1981)

    Article  Google Scholar 

  17. J. Katz, A. Plotkin, Low-Speed Aerodynamics (Cambridge University Press, Cambridge, 2001)

    Book  Google Scholar 

  18. J. Williams, L. Hall, Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane. J. Fluid Mech. 40(4), 657–670 (1970)

    Article  Google Scholar 

  19. N. Curle, The influence of solid boundaries upon aerodynamic sound. Proc. R. Soc. A 231(1187), 505–514 (1955)

    Article  MathSciNet  Google Scholar 

  20. M. Potter, J. Foss, Fluid Mechanics (Great Lakes Press, Okemos, MI, 1982)

    Google Scholar 

  21. S. Hoerner, Fluid-Dynamic Drag (Self-Published, New York, 1965)

    Google Scholar 

  22. S. Yarusevych, P. Sullivan, J. Kawall, On vortex shedding from an airfoil in low-Reynolds-number flows. J. Fluid Mech. 632, 245–271 (2009)

    Article  Google Scholar 

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Correspondence to Aren M. Hellum .

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© 2018 This is a U.S. government work and not under copyright protection in the U.S.; foreign copyright protection may apply

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Hellum, A.M. (2018). Acoustics of a Mixed Porosity Felt Airfoil. In: Ruffa, A., Toni, B. (eds) Advanced Research in Naval Engineering. STEAM-H: Science, Technology, Engineering, Agriculture, Mathematics & Health. Springer, Cham. https://doi.org/10.1007/978-3-319-95117-1_2

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