Effect of Inflow Conditions on the Noise Reduction Through Leading Edge Serrations
2019; American Institute of Aeronautics and Astronautics; Volume: 57; Issue: 9 Linguagem: Inglês
10.2514/1.j057831
ISSN1533-385X
AutoresTill M. Biedermann, Pasquale Czeckay, Thomas Geyer, Frank Kameier, Christian Oliver Paschereit,
Tópico(s)Fluid Dynamics and Turbulent Flows
ResumoNo AccessTechnical NotesEffect of Inflow Conditions on the Noise Reduction Through Leading Edge SerrationsTill M. Biedermann, Pasquale Czeckay, Thomas F. Geyer, Frank Kameier and Christian O. PaschereitTill M. BiedermannDusseldorf University of Applied Sciences, D-40476 Dusseldorf, Germany*Doctoral Researcher, Institute of Sound and Vibration Engineering (ISAVE); . Student Member AIAA.Search for more papers by this author, Pasquale CzeckayDusseldorf University of Applied Sciences, D-40476 Dusseldorf, Germany†Research Assistant, Institute of Sound and Vibration Engineering (ISAVE); .Search for more papers by this author, Thomas F. GeyerBrandenburg University of Technology Cottbus–Senftenberg, D-03046 Cottbus, Germany‡Research Associate, Aeroacoustics Research Group; . Member AIAA.Search for more papers by this author, Frank KameierDusseldorf University of Applied Sciences, D-40476 Dusseldorf, Germany§Professor, Institute of Sound and Vibration Engineering (ISAVE); .Search for more papers by this author and Christian O. PaschereitBerlin Technical University, D-10623 Berlin, Germany¶Professor, Institute of Fluid Dynamics and Technical Acoustics (ISTA); .Search for more papers by this authorPublished Online:24 Jun 2019https://doi.org/10.2514/1.J057831SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Kim J. W., Haeri S. and Joseph P. F., “On the Reduction of Aerofoil–Turbulence Interaction Noise Associated with Wavy Leading Edges,” Journal of Fluid Mechanics, Vol. 792, April 2016, pp. 526–552. doi:https://doi.org/10.1017/jfm.2016.95 CrossrefGoogle Scholar[2] Turner J. M. and Kim J. W., “Aeroacoustic Source Mechanisms of a Wavy Leading Edge Undergoing Vortical Disturbances,” Journal of Fluid Mechanics, Vol. 811, Jan. 2017, pp. 582–611. doi:https://doi.org/10.1017/jfm.2016.785 CrossrefGoogle Scholar[3] Chaitanya P., Joseph P., Narayanan S. and Kim J. W., “Aerofoil Broadband Noise Reductions Through Double-Wavelength Leading-Edge Serrations: A New Control Concept,” Journal of Fluid Mechanics, Vol. 855, Nov. 2018, pp. 131–151. doi:https://doi.org/10.1017/jfm.2018.620 CrossrefGoogle Scholar[4] Ayton L. J. and Kim J. W., “An Analytic Solution for the Noise Generated by Gust-Aerofoil Interaction for Plates with Serrated Leading Edges,” Journal of Fluid Mechanics, Vol. 853, Oct. 2018, pp. 515–536. doi:https://doi.org/10.1017/jfm.2018.583 CrossrefGoogle Scholar[5] Biedermann T. M., Chong T. P., Kameier F. and Paschereit C. O., “Statistical-Empirical Modelling of Airfoil Noise Subjected to Leading Edge Serrations,” AIAA Journal, Vol. 55, No. 9, 2017, pp. 3128–3142. doi:https://doi.org/10.2514/1.J055633 LinkGoogle Scholar[6] Ayton L. J. and Chaitanya P., “Analytic Solutions for Reduced Leading-Edge Noise Aerofoils,” 24th AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2018-3284, 2018. doi:https://doi.org/10.2514/6.2018-3284 LinkGoogle Scholar[7] Zhang M. and Frendi A., “Effect of Airfoil Leading Edge Waviness on Flow Structures and Noise,” International Journal of Numerical Methods for Heat & Fluid Flow, Vol. 26, No. 6, 2016, pp. 1821–1842. doi:https://doi.org/10.1108/HFF-04-2015-0143 CrossrefGoogle Scholar[8] Biedermann T., Kameier F., Koster O., Schreiber D., Chong T. P. and Paschereit C. O., “Polyoptimisation of the Aerodynamic and Aeroacoustic Performance of Aerofoils with Serrated Leading Edges,” 23rd AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2017-3493, 2017. doi:https://doi.org/10.2514/6.2017-3493 LinkGoogle Scholar[9] Juknevicius A., Chong T. P. and Woodhead P. C., “Leading Edge Noise Reduction of Thin Aerofoil by the Straight and Curved Serrations of the Add-On Type,” 23rd AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2017-3491, 2017. doi:https://doi.org/10.2514/6.2017-3491 LinkGoogle Scholar[10] Woodhead P. C., Chong T. P. and Wissink J., “Exploiting the Misalignment of the Serrated Trailing Edge for Improved Aerofoil Broadband Noise Reduction,” 23rd AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2017-4175, 2017. doi:https://doi.org/10.2514/6.2017-4175 LinkGoogle Scholar[11] Chaitanya P., Joseph P. and Ayton L., “On the Superior Performance of Leading Edge Slits over Serrations for the Reduction of Aerofoil Interaction Noise,” 24th AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2018-2018, 2018. doi:https://doi.org/10.2514/6.2018-3121.c1 Google Scholar[12] Turner J. and Kim J. W., “Towards Understanding Aerofoils with Wavy Leading Edges Interacting with Vortical Disturbances,” 22nd AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2016-2952, 2016. doi:https://doi.org/10.2514/6.2016-2952 LinkGoogle Scholar[13] Chaitanya P., Narayanan S., Joseph P., Vanderwel C., Kim J. W. and Ganapathisubramani B., “Broadband Noise Reduction Through Leading Edge Serrations on Realistic Aerofoils,” 21st AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2015-2202, 2015. doi:https://doi.org/10.2514/6.2015-2202 Google Scholar[14] Chen W., Qiao W., Wang L., Tong F. and Wang X., “Rod-Airfoil Interaction Noise Reduction Using Leading Edge Serrations,” 21st AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2015-3264, 2015. doi:https://doi.org/10.2514/6.2015-3264 LinkGoogle Scholar[15] Lyu B. and Azarpeyvand M., “On the Noise Prediction for Serrated Leading Edges,” Journal of Fluid Mechanics, Vol. 826, Sept. 2017, pp. 205–234. doi:https://doi.org/10.1017/jfm.2017.429 CrossrefGoogle Scholar[16] Narayanan S., Chaitanya P., Haeri S., Joseph P., Kim J. W. and Polacsek C., “Airfoil Noise Reductions Through Leading Edge Serrations,” Physics of Fluids, Vol. 27, No. 2, 2015, Paper 025109. doi:https://doi.org/10.1063/1.4907798 CrossrefGoogle Scholar[17] Clair V., Polacsek C., Le Garrec T., Reboul G., Gruber M. and Joseph P., “Experimental and Numerical Investigation of Turbulence-Airfoil Noise Reduction Using Wavy Edges,” AIAA Journal, Vol. 51, No. 11, 2013, pp. 2695–2713. doi:https://doi.org/10.2514/1.J052394 LinkGoogle Scholar[18] Geyer T., Sarradj E. and Giesler J., “Application of a Beamforming Technique to the Measurement of Airfoil Leading Edge Noise,” Advances in Acoustics and Vibration, Vol. 2012, No. 3, 2012, pp. 1–16. doi:https://doi.org/10.1155/2012/905461 CrossrefGoogle Scholar[19] Sarradj E., Fritzsche C., Geyer T. and Giesler J., “Acoustic and Aerodynamic Design and Characterization of a Small-Scale Aeroacoustic Wind Tunnel,” Applied Acoustics, Vol. 70, No. 8, 2009, pp. 1073–1080. doi:https://doi.org/10.1016/j.apacoust.2009.02.009 CrossrefGoogle Scholar[20] Sijtsma P., “CLEAN Based on Spatial Source Coherence,” 13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), AIAA Paper 2007-3436, 2007. doi:https://doi.org/10.2514/6.2007-3436 LinkGoogle Scholar[21] Sarradj E., “A Fast Ray Casting Method for Sound Refraction at Shear Layers,” International Journal of Aeroacoustics, Vol. 16, Nos. 1–2, 2017, pp. 65–77. doi:https://doi.org/10.1177/1475472X16680463 CrossrefGoogle Scholar[22] Herold G. and Sarradj E., “Performance Analysis of Microphone Array Methods,” Journal of Sound and Vibration, Vol. 401, Aug. 2017, pp. 152–168. doi:https://doi.org/10.1016/j.jsv.2017.04.030 CrossrefGoogle Scholar[23] Sarradj E., Herold G., Sijtsma P., Merino Martinez R., Geyer T. F., Bahr C. J., Porteous R., Moreau D. and Doolan C. J., “A Microphone Array Method Benchmarking Exercise Using Synthesized Input Data,” 23 AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2017-3719, 2017. doi:https://doi.org/10.2514/6.2017-3719 LinkGoogle Scholar[24] Bahr C. J., Humphreys W. M., Ernst D., Ahlefeldt T., Spehr C., Pereira A., Leclère Q., Picard C., Porteous R., Moreau D. and et al., “A Comparison of Microphone Phased Array Methods Applied to the Study of Airframe Noise in Wind Tunnel Testing,” 23rd AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2017-3718, 2017. doi:https://doi.org/10.2514/6.2017-3718 LinkGoogle Scholar[25] Hinze J. O., Turbulence, 2nd ed., McGraw–Hill, New York, 1987, Chap. 3. Google Scholar[26] Roach P. E., “The Generation of Nearly Isotropic Turbulence by Means of Grids,” International Journal of Heat and Fluid Flow, Vol. 8, No. 2, 1987, pp. 82–92. doi:https://doi.org/10.1016/0142-727X(87)90001-4 CrossrefGoogle Scholar[27] Schulz-Hausmann F. K., “Wechselwirkung ebener Freistrahlen mit der Umgebung,” Ph. D. Thesis, Institut für Thermo- und Fluiddynamik, Ruhr Universität Bochum, Bochum, Germany, 1985. Google Scholar[28] Van Nierop E. A., Alben S. and Brenner M. P., “How Bumps on Whale Flippers Delay Stall: An Aerodynamic Model,” Physical Review Letters, Vol. 100, No. 5, 2008, Paper 54502. doi:https://doi.org/10.1103/PhysRevLett.100.054502 CrossrefGoogle Scholar[29] Cai C., Zuo Z., Maeda T., Kamada Y., Li Q.’a., Shimamoto K. and Liu S., “Periodic and Aperiodic Flow Patterns Around an Airfoil with Leading-Edge Protuberances,” Physics of Fluids, Vol. 29, No. 11, 2017, Paper 115110. doi:https://doi.org/10.1063/1.4991596 CrossrefGoogle Scholar[30] Biedermann T. M., Czeckay P., Geyer T., Kameier F. and Paschereit C. O., “Noise Source Identification of Aerofoils Subjected to Leading Edge Serrations Using Phased Array Beamforming,” 24th AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2018-3794, 2018. doi:https://doi.org/10.2514/6.2018-3794 LinkGoogle Scholar[31] Chen J.-H., Li S.-S. and Nguyen V. T., “The Effect of Leading Edge Protuberances on the Performance of Small Aspect Ratio Foils,” 15th International Symposium on Flow Visualization, Luikov Heat and Mass Transfer Institute (HMTI), Belarus National Academy of Sciences, 2012. doi:https://doi.org/10.13140/RG.2.1.3716.7841 Google Scholar[32] Guerreiro J. L. E. and Sousa J. M. M., “Low-Reynolds-Number Effects in Passive Stall Control Using Sinusoidal Leading Edges,” AIAA Journal, Vol. 50, No. 2, 2012, pp. 461–469. doi:https://doi.org/10.2514/1.J051235 LinkGoogle Scholar[33] Chaitanya P., Joseph P., Narayanan S., Vanderwel C., Turner J., Kim J. W. and Ganapathisubramani B., “Performance and Mechanism of Sinusoidal Leading Edge Serrations for the Reduction of Turbulence–Aerofoil Interaction Noise,” Journal of Fluid Mechanics, Vol. 818, May 2017, pp. 435–464. doi:https://doi.org/10.1017/jfm.2017.141 CrossrefGoogle Scholar[34] Oerlemans S. and Migliore P., “Aeroacoustic Wind Tunnel Tests of Wind Turbine Airfoils,” 10th AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2004-3042, 2004. doi:https://doi.org/10.2514/6.2004-3042 LinkGoogle Scholar[35] Carolus T., Ventilatoren, Vieweg+Teubner Verlag, Wiesbaden, 2013, Chap. 4.3. CrossrefGoogle Scholar[36] Blake W. K., Mechanics of Flow-Induced Sound and Vibration, Vol. 2, Complex Flow-Structure Interactions, 2nd ed., Elsevier Science, San Diego, 2017, Chap. 5.2. Google Scholar[37] Chong T. P., Biedermann T., Koster O. and Hasheminejad S. M., “On the Effect of Leading Edge Serrations on Aerofoil Noise Production,” 24th AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2018-3289, 2018. doi:https://doi.org/10.2514/6.2018-3289 LinkGoogle Scholar[38] Hansen K., Kelso R. and Doolan C., “Reduction of Flow Induced Tonal Noise Through Leading Edge Tubercle Modifications,” 16th AIAA/CEAS Aeroacoustics Conference, AIAA Paper 2010-3700, 2010. doi:https://doi.org/10.2514/6.2010-3700 LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byOn the interactions of the induced flow field of heat exchangers with axial fansExperimental Thermal and Fluid Science, Vol. 139Aerodynamic and aeroacoustic properties of axial fan blades with slitted leading edges25 October 2022 | Acta Acustica, Vol. 6Permeable Leading Edges for Airfoil and Fan Noise Reduction in Disturbed InflowChristof Ocker , Thomas F. Geyer, Felix Czwielong, Florian Krömer, Wolfram Pannert, Markus Merkel and Stefan Becker2 August 2021 | AIAA Journal, Vol. 59, No. 12Effect of geometric parameters on the noise generated by rod-airfoil configurationApplied Acoustics, Vol. 177Towards the Understanding of Humpback Whale Tubercles: Linear Stability Analysis of a Wavy Flat Plate19 November 2020 | Fluids, Vol. 5, No. 4Applicability of Aeroacoustic Scaling Laws of Leading Edge Serrations for Rotating Applications23 July 2020 | Acoustics, Vol. 2, No. 3On the use of leading-edge serrations for noise control in a tandem airfoil configurationPhysics of Fluids, Vol. 32, No. 7Experimental Investigation of the Impact of 3D-Metal-Printed Perforated Leading Edges on Airfoil and Axial Fan NoiseChristof Ocker, Thomas F. Geyer, Felix Czwielong, Florian Krömer, Stefan Becker, Markus Merkel and Wolfram Pannert8 June 2020 What's Popular Volume 57, Number 9September 2019Special Section on Advances in Bio-inspired Propulsion CrossmarkInformationCopyright © 2019 by Till M. Biedermann, P. Czeckay, T. Geyer. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAeroacousticsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsBoundary LayersFlow RegimesFluid DynamicsTurbulenceVortex DynamicsWind Tunnels KeywordsLift to Drag RatioSound Pressure LevelFree Stream VelocityStrouhal NumberAerodynamic PerformanceTurbulent Boundary LayerTurbulence Length ScaleTurbulence IntensityVortex GeneratorsAirfoil ChordAcknowledgmentThe authors gratefully acknowledge T. P. Chong from Brunel University London for generously providing some of the hardware needed for the study.PDF Received15 August 2018Accepted17 May 2019Published online24 June 2019
Referência(s)