Effect of Porous Surface on the Flat Plate Self-Noise

In this study, the effect of porous surface on the turbulent noise generated by a blunt trailing-edge of a flat plate is investigated. The three-dimensional turbulent flow over the flat plate (Rec=1.3×10 5 and M=0.06) is computed by incompressible large eddy simulation (LES) based on the volume-averaged Navier-Stokes equations, while the acoustic field is calculated by the linearized perturbed compressible equations (LPCE) coupled with LES solutions. The porous surface is applied to a small, selected area near the trailing-edge, where the Karman vortex shedding and eddy scattering produce dipole sounds. The computed results show that the trailing-edge with porosity e=0.25 and permeability (normalized) K * =0.01 yields a reduction of tonal peak by 13dB for zero angle of attack (α=0o), via breaking not only in the streamwise direction but also in the spanwise direction the spatial correlation of the wall pressure fluctuations (Rpp) near the trailing-edge. For the separated flow case (α=5o), the same configuration of the porous surface is found to weaken the pressure fluctuations at the trailing edge. It results in 3-10dB noise reduction over a wide range of frequency, via reducing the separated flow region over the upper surface of the plate.

[1]  S. Ergun Fluid flow through packed columns , 1952 .

[2]  J. Williams,et al.  Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane , 1970, Journal of Fluid Mechanics.

[3]  M. S. Howe A review of the theory of trailing edge noise , 1978 .

[4]  T. Brooks,et al.  Trailing edge noise prediction from measured surface pressures , 1981 .

[5]  S. Lele Compact finite difference schemes with spectral-like resolution , 1992 .

[6]  H. Fujita,et al.  Numerical prediction of aerodynamic noise radiated from low Mach number turbulent wake , 1993 .

[7]  Soogab Lee Reduction of blade-vortex interaction noise through porous leading edge , 1994 .

[8]  S. Whitaker The Forchheimer equation: A theoretical development , 1996 .

[9]  Anthony R. Pilon,et al.  A numerical investigation of noise from a rectangular jet , 1997 .

[10]  Shelly S. Sadowski,et al.  Investigation of high-lift flow field of an energy efficient transport wing , 1999 .

[11]  Jeffrey L. Young,et al.  Practical aspects of higher-order numerical schemes for wave propagation phenomena , 1999 .

[12]  Mehdi R. Khorrami,et al.  Investigation of High-Lift Flowfield of an Energy Efficient Transport Wing , 2000 .

[13]  S. B. Khelil,et al.  Numerical prediction of the unsteady flow and radiated noise from a 3D lifting airfoil , 2001 .

[14]  Meelan Choudhari,et al.  A novel approach for reducing rotor tip-clearance induced noise in turbofan engines , 2001 .

[15]  A Boundary Condition for Simulation of Flow Over Porous Surfaces , 2001 .

[16]  Meelan Choudhari,et al.  Application of Passive Porous Treatment to Slat Trailing Edge Noise , 2003 .

[17]  Meelan Choudhari,et al.  Computational Study of Porous Treatment for Altering Flap Side-Edge Flowfield , 2003 .

[18]  C. Bailly,et al.  Numerical Prediction of the Noise Radiated by a Cylinder , 2003 .

[19]  David P. Lockard,et al.  The Airframe Noise Reduction Challenge , 2004 .

[20]  I. Mortazavi,et al.  Passive control of the flow around a square cylinder using porous media , 2004 .

[21]  Michel Roger,et al.  Broadband Self Noise from Loaded Fan Blades , 2004 .

[22]  W. Schröder,et al.  On the simulation of trailing edge noise with a hybrid LES/APE method , 2004 .

[23]  J. Seo,et al.  Prediction of Low Mach Number Turbulent Flow Noise Using the Splitting Method , 2004 .

[24]  Michaela Herr,et al.  Experimental investigations in low-noise trailing-edge design , 2004 .

[25]  J. Seo,et al.  The linearized perturbed compressible equations for aeroacoustic noise prediction at very low Mach numbers , 2005 .

[26]  J. Seo,et al.  Perturbed Compressible Equations for Aeroacoustic Noise Prediction at Low Mach Numbers , 2005 .

[27]  B. Boersma,et al.  Direct numerical simulations of turbulent flow over a permeable wall using a direct and a continuum approach , 2005 .

[28]  Jung Hee Seo,et al.  Linearized perturbed compressible equations for low Mach number aeroacoustics , 2006, J. Comput. Phys..

[29]  J. Seo,et al.  Prediction of flat plate self-noise , 2006 .

[30]  J. Dennis,et al.  Trailing-edge noise reduction using derivative-free optimization and large-eddy simulation , 2007, Journal of Fluid Mechanics.

[31]  J. Seo,et al.  Aerodynamic noise prediction for long-span bodies , 2007 .