Fan Noise Prediction: Status and Needs

The prediction of fan noise is an important part to the prediction of overall turbofan engine noise. Advances in computers and better understanding of the flow physics have allowed researchers to compute sound generation from first principles and rely less on empirical correlations. While progress has been made, there are still many aspects of the problem that need to be explored. This paper presents some recent advances in fan noise prediction and suggests areas that still need further development. Fan noise predictions that support the recommendations are taken from existing publications.

[1]  Masanobu Namba Three-dimensional analysis of blade force and sound generation for an annular cascade in distorted flows , 1977 .

[2]  T. G. Sofrin,et al.  Axial Flow Compressor Noise Studies , 1962 .

[3]  Joannes Bernardus Henricus Maria Schulten,et al.  Sound generation by ducted fans and propellers as a lifting surface problem , 1993 .

[4]  R. Martinez,et al.  NUMERICAL PREDICTIONS OF DIFFRACTION OF BROADBAND NOISE BY AN ENGINE NACELLE; PART I: CALCULATION OF A STATOR CASCADE'S NEAR- AND FARFIELD RADIATIONS FROM THE INGESTION OF RAPIDLY DISTORTING TURBULENCE , 1997 .

[5]  W. D. Mark,et al.  Turbofan noise generation. Volume 1: Analysis , 1982 .

[6]  M. M. Rai,et al.  A numerical analysis of tonal acoustics in rotor-stator interactions , 1993 .

[7]  Joseph M. Verdon,et al.  Review of unsteady aerodynamic methods for turbomachinery aeroelastic and aeroacoustic applications , 1993 .

[8]  D. Topol Development of a fan noise design system. II - Far-field radiation and system evaluation , 1993 .

[9]  James Bridges,et al.  Comparison of Predicted Low Speed Fan Rotor/Stator Interaction Modes to Measured , 1997 .

[10]  D. Topol,et al.  Development of a fan noise design system. I - Design system and source modeling , 1993 .

[11]  V. Golubev,et al.  Acoustic-vorticity modes in an annular duct with mean vortical swirling flow , 1997 .

[12]  Kenneth C. Hall,et al.  Sensitivity Analysis of the Aeroacoustic Response of Turbomachinery Blade Rows , 1995 .

[13]  Walter Eversman,et al.  Ducted fan acoustic radiation including the effects of nonuniform mean flow and acoustic treatment , 1993 .

[14]  S. J. Horowitz,et al.  An iterative finite element-integral technique for predicting sound radiation from turbofan inlets in steady flight , 1982 .

[15]  Hafiz M. Atassi,et al.  Numerical Solutions for Unsteady Subsonic Vortical Flows Around Loaded Cascades , 1992 .

[16]  Thomas F. Brooks,et al.  Airfoil self-noise and prediction , 1989 .

[17]  P. R. Gliebe The effect of throttling on forward radiated fan noise , 1979 .

[18]  Robert P. Dougherty,et al.  A Wave-Splitting Technique for Nacelle Acoustic Propagation , 1997 .

[19]  J. Bridges,et al.  A unique ducted fan test bed for active noise control and aeroacoustics research , 1996 .

[20]  S. J. Horowitz,et al.  Finite Element-Integral Acoustic Simulation of JT15D Turbofan Engine , 1984 .

[21]  J. Verdon,et al.  A Three-Dimensional Linearized Unsteady Euler Analysis for Turbomachinery Blade Rows , 1996 .

[22]  P. Spence Ducted fan noise prediction using wave envelope analysis and the Kirchhoff formula , 1997 .

[23]  Donald Hanson Acoustic reflection and transmission of rotors and stators including mode and frequency scattering , 1997 .

[24]  Edward Rademaker,et al.  Experimental Validation of Lifting Surface Theory for Rotor-Stator Interaction Noise Generation , 1998 .

[25]  Harvey H. Hubbard,et al.  Aeroacoustics of Flight Vehicles: Theory and Practice , 1994 .

[26]  H. Meyer Effect of inlet reflections on fan noise radiation , 1996 .

[27]  G. Hamad,et al.  Sound generated in a cascade by three-dimensional disturbances convected in a subsonic flow , 1981 .

[28]  Edward A. Prydz Rice Multimodal Far-Field Acoustic Radiation Pattern Using Mode Cutoff Ratio , 1978 .

[29]  S. D. Savkar,et al.  Radiation of cylindrical duct acoustic modes with flow mismatch. [effects on aircraft engine noise] , 1975 .

[30]  David A. Topol DEVELOPMENT AND EVALUATION OF A COUPLED FAN NOISE DESIGN SYSTEM , 1997 .

[31]  H. Atassi,et al.  Sound radiated from a loaded cascade in nonuniform transonic flow , 1996 .

[32]  S. Kaji,et al.  Generation of sound by rotor-stator interaction , 1970 .

[33]  Edmane Envia,et al.  Aeroacoustic Analysis of Turbofan Noise Generation , 1996 .

[34]  M. Nallasamy,et al.  Azimuthal Directivity of Fan Tones Containing Multiple Modes , 1997 .

[35]  R. K. Majjigi,et al.  Development of a rotor wake-vortex model, volume 1 , 1984 .

[36]  Stewart A. L. Glegg,et al.  Broadband Self-Noise from a Ducted Fan , 1998 .

[37]  Laurence J. Heidelberg,et al.  Inlet acoustic mode measurements using a continuously rotating rake , 1995 .

[38]  Stewart A. L. Glegg,et al.  Airfoil Self-Noise Generated in a Cascade , 1998 .

[39]  Walter Eversman,et al.  Aft Fan Duct Acoustic Radiation , 1998 .

[40]  John K. C. Low Ultra-High Bypass Ratio Jet Noise , 1994 .

[41]  Philip R. Gliebe,et al.  UHB Engine Fan Broadband Noise Reduction Study , 1995 .

[42]  Christopher L. Rumsey,et al.  Computation of acoustic waves through sliding-zone interfaces using an Euler/Navier-Stokes code , 1996 .

[43]  S. Kaji Noncompact source effect on the prediction of tone noise from a fan rotor , 1975 .

[44]  J. C. Hardin,et al.  Second Computational Aeroacoustics (CAA) Workshop on Benchmark Problems , 1997 .

[45]  H. Kobayashi,et al.  Three-dimensional effects on pure tone fan noise due to inflow distortion , 1978 .