A 3D analytical model for orthogonal blade-vortex interaction noise

Abstract A 3D analytical model of an Orthogonal Blade-Vortex Interaction (OBVI) for Counter-Rotating Open Rotor (CROR) tonal noise is investigated. The specific influence of two parameters taking into account the three-dimensionality of both the vortex velocity and the convection velocity within the rotor-rotor volume is addressed. The first step is to extract the vortex parameters from a recent unsteady Reynolds-Averaged Navier-Stokes computation and validate different vortex models. Lamb-Oseen and Scully vortices reproduce the behavior of the tip-vortex tangential velocity fairly well. Regarding the vortex axial velocity modeling, a Gaussian profile fits well with numerical results. On the one hand, the impact of the stream-tube contraction unbalances the lobes of the unsteady pressure with opposite phases produced by the OBVI event. This effect is larger than that of an equivalent blade sweep. On the other hand, adding the axial velocity deficit to the tangential one also unbalances the pressure lobes. Finally, from an acoustic point of view using Curle's acoustic analogy, both the stream-tube contraction and the axial velocity deficit have the same effect: they turn an acoustically-low efficient quadrupole into a strong dipole making these parameters fundamental for future CROR OBVI investigations.

[1]  N. Curle The influence of solid boundaries upon aerodynamic sound , 1955, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.

[2]  S. Moreau,et al.  A 3D analytical approach for Open rotor Blade Vortex Interaction(BVI) tonal noise , 2015 .

[3]  Roger C. Strawn,et al.  Computer Visualization Of Vortex Wake Systems , 1998 .

[4]  Rod Self,et al.  Counter-Rotation Propeller Tip Vortex Interaction Noise , 2009 .

[5]  Gregory Delattre,et al.  Investigation of Counter Rotating Open Rotor Orthogonal Blade/Vortex Interaction Noise , 2014 .

[6]  I. S. Gradshteyn,et al.  Table of Integrals, Series, and Products , 1976 .

[7]  Richard P. Woodward,et al.  An Open Rotor Test Case: F31/A31 Historical Baseline Blade Set , 2011 .

[8]  J. H. Dittmar,et al.  Some design philosophy for reducing the community noise of advanced counter-rotation propellers , 1985 .

[9]  Richard P. Woodward,et al.  Measured noise of a scale model high speed propeller at simulated takeoff/approach conditions , 1987 .

[10]  Rasika Fernando,et al.  Open-Rotor low speed aero-acoustics: wind tunnel characterization of an advanced blade design in isolated and installed configurations , 2014 .

[11]  Dale E. Van Zante,et al.  Tip Vortex and Wake Characteristics of a Counterrotating Open Rotor , 2012 .

[12]  Johan C. Kok,et al.  Resolving the Dependence on Freestream Values for the k- Turbulence Model , 2000 .

[13]  M. Liou A Sequel to AUSM , 1996 .

[14]  Gregory Delattre,et al.  Influence of Torque Ratio on Counter-Rotating Open-Rotor Interaction Noise , 2014 .

[15]  R. K. Majjigi,et al.  An investigation of counterrotating tip vortex interaction , 1989 .

[16]  Zoltán S. Spakovszky,et al.  Rotor Interaction Noise in Counter-Rotating Propfan Propulsion Systems , 2012 .

[17]  M. Scully,et al.  Computation of helicopter rotor wake geometry and its influence on rotor harmonic airloads , 1975 .

[18]  Joseph Lipka,et al.  A Table of Integrals , 2010 .

[19]  F. N. Cotona,et al.  Helicopter Tail Rotor Orthogonal Blade Vortex Interaction , 2004 .

[20]  K. Schwarzschild,et al.  Die Beugung und Polarisation des Lichts durch einen Spalt. I , 1901 .

[21]  Hans-Peter Kau,et al.  Aerodynamic Origin of Rotor-Rotor Interaction Noise From Unducted Propulsors , 2013 .

[22]  Michel Roger,et al.  Analytical Prediction of Wake-Interaction Noise in Counter-Rotating Open Rotors , 2011 .

[23]  Stéphane Moreau,et al.  On vortex–airfoil interaction noise including span-end effects, with application to open-rotor aeroacoustics , 2014 .

[25]  Michel Roger On broadband jet–ring interaction noise and aerofoil turbulence-interaction noise predictions , 2010, Journal of Fluid Mechanics.

[26]  Michel Roger,et al.  Effect of Angle of Attack and Airfoil Shape on Turbulence-Interaction Noise , 2005 .

[27]  R. K. Amiet,et al.  High frequency thin-airfoil theory for subsonic flow , 1976 .

[28]  Stéphane Moreau,et al.  Assessment and comparison of tonal noise models for Counter-Rotating Open Rotors , 2013 .

[29]  John J. Adamczyk,et al.  Passage of a Swept Airfoil through an Oblique Gust , 1974 .

[30]  D. B. Stang,et al.  Reduction of the noise of a model counterrotation propeller at cruise by reducing the aft propeller diameter , 1987 .

[31]  J. H. Dittmar Cruise noise of counterrotation propeller at angle of attack in wind tunnel , 1986 .

[32]  S. Lin,et al.  Theoretical and experimental studies on vortex chamber flows , 1986 .

[33]  J. Marshall,et al.  Blade penetration into a vortex core with and without axial core flow , 2004, Journal of Fluid Mechanics.

[34]  S. Moreau,et al.  Numerical assessment of the noise emission of counter-rotating open rotors , 2013 .

[35]  S. Moreau,et al.  Numerical assessment of the tonal noise of Counter-Rotating Open Rotors at approach , 2016 .

[36]  F. Menter Improved two-equation k-omega turbulence models for aerodynamic flows , 1992 .

[37]  James C. McWilliams,et al.  Barotropic and Baroclinic Instabilities of Axisymmetric Vortices in a Quasigeostrophic Model , 1989 .

[38]  H. Squire The Growth of a Vortex in Turbulent Flow , 1965 .

[39]  Farhan Gandhi,et al.  A Critical Evaluation of Various Approaches for the Numerical Detection of Helicopter Blade-Vortex Interactions , 2000 .

[40]  Michel Roger,et al.  Competing Broadband Noise Mechanisms in Low-Speed Axial Fans , 2004 .

[41]  Richard P. Woodward,et al.  Noise of a model counterrotation propeller with reduced aft rotor diameter at simulated takeoff/approach conditions (F7/A3) , 1988 .

[42]  Jinhee Jeong,et al.  On the identification of a vortex , 1995, Journal of Fluid Mechanics.

[43]  Julien Christophe,et al.  Application of hybrid methods to high frequency aeroacoustics , 2011 .

[44]  Michel Roger,et al.  Back-scattering correction and further extensions of amiet's trailing-edge noise model. Part 1: theory , 2005 .

[45]  Irene A. Stegun,et al.  Handbook of Mathematical Functions. , 1966 .

[46]  Gregory Delattre,et al.  Counter-Rotating Open Rotor (CROR) : flow physics and simulation , 2011 .

[47]  F. Menter ZONAL TWO EQUATION k-w TURBULENCE MODELS FOR AERODYNAMIC FLOWS , 1993 .

[48]  Michel Roger,et al.  Blade-Geometry Considerations in Analytical Gust-Airfoil Interaction Noise Models , 2010 .