Similarities of the free-field and in-duct formulations in rotor noise problems

This paper deals with the comparison between open rotor and ducted fan noise. Similar theoretical formulations for the freeeld and in-duct noise problems are derived from the original equation for noise generation given by Goldstein. The form of the nal equations enables to separate the terms related to noise propagation from those representing the acoustic source. Among the similarities shared by the freeeld and in-duct cases, the possibility to de ne a common cut-o ratio for the spinning modes provides some insight in the relation between the position of the sources and the excited modes in a way more general than that already proposed by the authors. With help of this formalism we hope to reach a better understanding of the di erences in noise levels to be expected on contrarotating open rotor (CROR) and contra-rotating turbofan (CRTF) concepts.

[1]  Stewart A. L. Glegg Broadband noise from ducted prop fans , 1993 .

[2]  W Ganz Ulrich,et al.  Boeing 18-Inch Fan Rig Broadband Noise Test , 1998 .

[3]  W. Sears,et al.  Some Aspects of Non-Stationary Airfoil Theory and Its Practical Application , 1941 .

[4]  Donald B. Hanson,et al.  Unified analysis of fan stator noise , 1973 .

[5]  D. B. Hanson,et al.  The importance of quadrupole sources in prediction of transonic tip speed propeller noise , 1978 .

[6]  Stéphane Moreau,et al.  Fan Trailing-Edge Noise Prediction Using RANS Simulations , 2010 .

[7]  R. Amiet Acoustic radiation from an airfoil in a turbulent stream , 1975 .

[8]  Brian J. Tester,et al.  An Analytic Green's Function for a Lined Circular Duct Containing Uniform Mean Flow , 2005 .

[9]  Sebastien Guerin,et al.  Development and application of a new procedure for fan noise prediction , 2010 .

[10]  D. B. Hanson,et al.  Near-field frequency-domain theory for propeller noise , 1985 .

[11]  Phillip Joseph,et al.  Determining the strength of rotating broadband sources in ducts by inverse methods , 2006 .

[12]  C. Morfey Acoustic energy in non-uniform flows , 1971 .

[13]  David B. Stephens,et al.  Sound Generation by a Rotor Interacting with a Casing Turbulent Boundary Layer , 2009 .

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

[15]  Hafiz M. Atassi,et al.  Fan Broadband Noise in Anisotropic Turbulence , 2009 .

[16]  D I Blokhintsev,et al.  Acoustics of a Nonhomogeneous Moving Medium. , 1956 .

[17]  G. Corcos The structure of the turbulent pressure field in boundary-layer flows , 1964, Journal of Fluid Mechanics.

[18]  Stéphane Moreau,et al.  Extensions and limitations of analytical airfoil broadband noise models , 2010 .

[19]  Donald J. Kee Hanson,et al.  Helicoidal Surface Theory for Harmonic Noise of Propellers in the Far Field , 1980 .

[20]  T. F. W. Embleton,et al.  Efficiency of Circular Sources and Circular Arrays of Point Sources with Linear Phase Variation , 1962 .

[21]  D. Crighton,et al.  An asymptotic theory of near-field propeller acoustics , 1991, Journal of Fluid Mechanics.

[22]  C. Tam,et al.  Jet Mixing Noise from Fine-Scale Turbulence , 1998 .

[23]  Cyrus D. Cantrell,et al.  Modern Mathematical Methods for Physicists and Engineers , 2000 .

[24]  J. B. H. M. Schulten,et al.  Frequency-Domain Method for the Computation of Propeller Acoustics , 1988 .

[25]  Donald B. Hanson Noise of counter-rotation propellers , 1985 .

[26]  C. L. Morfey,et al.  Sound transmission and generation in ducts with flow , 1971 .

[27]  F. Farassat,et al.  Prediction of advanced propeller noise in the time domain , 1986 .

[28]  D. Blokhintzev,et al.  The Propagation of Sound in an Inhomogeneous and Moving Medium I , 1946 .

[29]  R. Amiet Noise due to turbulent flow past a trailing edge , 1976 .

[30]  F. Holste Ermittlung der aerodynamischen Lärmquellen und Berechnung des abgestrahlten Schallfeldes mittels der im Nahfeld gemessenen Druckschwankungen am Beispiel eines Triebwerksmodells , 1995 .