Computation of the noise generated by low Mach number flows around a cylinder and a wall-mounted half-cylinder

For modern cars, aerodynamic noise is becoming the major source of annoyance during peri-urban trips. To take this point into consideration from the vehicle development and to improve the interior comfort, appropriate numerical methods have to be developed. The estimation of the broadband noise generated by low Mach number flows about M 0.1, considered in this study, are obtained by applying a two-step method combining incompressible CFD calculations with acoustic analogy. In this paper, the advanced-time algorithm is developed to allow the estimation of all the terms of Ffowcs Williams and Hawkings’ equation and particularly the volume terms. The noise corresponding to a cylinder flow is then used to validate this approach and to compute the broadband noise radiated by a 3-D incompressible and turbulent flow. The algorithm is then applied to a wall-mounted half-cylinder corresponding to a simplified side-mirror shape. In order to validate the half-cylinder aeroacoustic calculations, the numerical results are favourably compared to measurements recently carried out.

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

[2]  P. D. Francescantonio A NEW BOUNDARY INTEGRAL FORMULATION FOR THE PREDICTION OF SOUND RADIATION , 1997 .

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

[4]  C. Bogey,et al.  Noise Investigation of a High Subsonic, Moderate Reynolds Number Jet Using a Compressible Large Eddy Simulation , 2003 .

[5]  M. S. Howe Acoustics of Fluid–Structure Interactions: Index , 1998 .

[6]  HighWire Press Philosophical Transactions of the Royal Society of London , 1781, The London Medical Journal.

[7]  Xavier Gloerfelt,et al.  Direct computation of the noise radiated by a subsonic cavity flow and application of integral methods , 2003 .

[8]  A. Powell Aerodynamic Noise and the Plane Boundary , 1960 .

[9]  S. Lee A LARGE-EDDY SIMULATION OF THE TURBULENT FLOW IN THE VICINITY OF AN UPRIGHT WALL-MOUNTED HALF CYLINDER AND AERODYNAMIC SOUND PREDICTION , 2002 .

[10]  B. Cantwell,et al.  An experimental study of entrainment and transport in the turbulent near wake of a circular cylinder , 1983, Journal of Fluid Mechanics.

[11]  U. Piomelli,et al.  Wall-layer models for large-eddy simulations , 2008 .

[12]  A. Runchal,et al.  A LARGE-EDDY SIMULATION OF THE TURBULENT FLOW IN THE VICINITY OF AN UPRIGHT WALL-MOUNTED HALF CYLINDER AND AERODYNAMIC SOUND PREDICTION , 1999 .

[13]  J. Batham,et al.  Pressure distributions on circular cylinders at critical Reynolds numbers , 1973, Journal of Fluid Mechanics.

[14]  M. Breuer A CHALLENGING TEST CASE FOR LARGE EDDY SIMULATION: HIGH REYNOLDS NUMBER CIRCULAR CYLINDER FLOW , 2000, Proceeding of First Symposium on Turbulence and Shear Flow Phenomena.

[15]  D. G. Crighton,et al.  On the scattering of aerodynamic noise , 1971 .

[16]  F. Tremblay Direct and large-eddy simulation of flow around a circular cylinder at subcritical Reynolds numbers , 2002 .

[17]  C. Bogey,et al.  A family of low dispersive and low dissipative explicit schemes for flow and noise computations , 2004 .

[18]  P. Moin,et al.  Approximate Wall Boundary Conditions in the Large-Eddy Simulation of High Reynolds Number Flow , 2000 .

[19]  D. L. Hawkings,et al.  Sound generation by turbulence and surfaces in arbitrary motion , 1969, Philosophical Transactions of the Royal Society of London. Series A, Mathematical and Physical Sciences.

[20]  Parviz Moin,et al.  Computation of quadrupole noise using acoustic analogy , 1996 .

[21]  Michael Manhart,et al.  LES OF FLOW AROUND A CIRCULAR CYLINDER AT A HIGH SUBCRITICAL REYNOLDS NUMBER , 2001 .

[22]  F. Farassat,et al.  Modeling aerodynamically generated sound of helicopter rotors , 2003 .