A comparison between measured and predicted fan broadband noise due to rotor-stator interaction
A comparison between measured and predicted fan broadband noise due to rotor-stator interaction
 
  This paper presents a comparison between predictions and measurements of the broad-band noise generated in a low-speed fan rig. It is assumed here that the dominant generation mechanism is due to rotor-stator interaction. In the broadband noise model the stator is modelled as a cascade of flat plate airfoils on which turbulent wakes due to the rotor impinge. The turbulence transverse length scale and intensity of the rotor wake are determined by data from measurement and RANS calculations. The theoretical expression for the acoustic power spectra is shown to be in the form of the product of an aerodynamic response function and the spectrum of the velocity fluctuations normal to the stator blade direction. The response function is obtained by solving numerically an aerodynamic integral equation, while the turbulence velocity spectrum is expressed analytically in a form similar to an isotropic homogeneous turbulence model. The turbulence is also modelled by random velocity fluctuations superimposed on a statistic distribution of the rms velocity. The statistical distribution is composed of a constant term, modelling the background turbulence and a periodic Gaussian-profile to represent the rotor-wake turbulence. Extensive hot wire measurements of both the steady and unsteady wake velocity was measured. Comparisons between these measurements and RANS predictions are also presented.
  
    
      Jurdic, V.
      
        37a5b11b-d9c0-4cb9-8930-532988d27007
      
     
  
    
      Moreau, A.
      
        e7ef260e-7129-4ec2-9e47-9b915cab09fe
      
     
  
    
      Joseph, P.F.
      
        9c30491e-8464-4c9a-8723-2abc62bdf75d
      
     
  
    
      Enghardt, L.J.
      
        233ae9d1-d93e-4d59-97d1-96dba1dd23db
      
     
  
    
      Coupland, J.
      
        f0429ea4-fe7f-42df-b6fd-fd2e1446412f
      
     
  
  
   
  
  
    
      May 2007
    
    
  
  
    
      Jurdic, V.
      
        37a5b11b-d9c0-4cb9-8930-532988d27007
      
     
  
    
      Moreau, A.
      
        e7ef260e-7129-4ec2-9e47-9b915cab09fe
      
     
  
    
      Joseph, P.F.
      
        9c30491e-8464-4c9a-8723-2abc62bdf75d
      
     
  
    
      Enghardt, L.J.
      
        233ae9d1-d93e-4d59-97d1-96dba1dd23db
      
     
  
    
      Coupland, J.
      
        f0429ea4-fe7f-42df-b6fd-fd2e1446412f
      
     
  
       
    
 
  
    
      
  
  
  
  
    Jurdic, V., Moreau, A., Joseph, P.F., Enghardt, L.J. and Coupland, J.
  
  
  
  
   
    (2007)
  
  
    
    A comparison between measured and predicted fan broadband noise due to rotor-stator interaction.
  
  
  
  
    
    
    
      
        
   
  
    13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), , Rome, Italy.
   
        
        
        20 - 22  May 2007.
      
    
  
  
  
      
          
           17 pp
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      Record type:
      Conference or Workshop Item
      (Paper)
      
      
    
   
    
      
        
          Abstract
          This paper presents a comparison between predictions and measurements of the broad-band noise generated in a low-speed fan rig. It is assumed here that the dominant generation mechanism is due to rotor-stator interaction. In the broadband noise model the stator is modelled as a cascade of flat plate airfoils on which turbulent wakes due to the rotor impinge. The turbulence transverse length scale and intensity of the rotor wake are determined by data from measurement and RANS calculations. The theoretical expression for the acoustic power spectra is shown to be in the form of the product of an aerodynamic response function and the spectrum of the velocity fluctuations normal to the stator blade direction. The response function is obtained by solving numerically an aerodynamic integral equation, while the turbulence velocity spectrum is expressed analytically in a form similar to an isotropic homogeneous turbulence model. The turbulence is also modelled by random velocity fluctuations superimposed on a statistic distribution of the rms velocity. The statistical distribution is composed of a constant term, modelling the background turbulence and a periodic Gaussian-profile to represent the rotor-wake turbulence. Extensive hot wire measurements of both the steady and unsteady wake velocity was measured. Comparisons between these measurements and RANS predictions are also presented.
        
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      Published date: May 2007
 
    
  
  
    
  
    
     
        Additional Information:
        AIAA 2007-3692
      
    
  
    
     
        Venue - Dates:
        13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference), , Rome, Italy, 2007-05-20 - 2007-05-22
      
    
  
    
  
    
     
    
  
    
  
    
  
    
  
  
  
    
  
    
  
  
        Identifiers
        Local EPrints ID: 50417
        URI: http://eprints.soton.ac.uk/id/eprint/50417
        
        
        
        
          PURE UUID: 35e3a56d-04fd-462a-885e-04e6e843409a
        
  
    
        
          
        
    
        
          
        
    
        
          
            
          
        
    
        
          
        
    
        
          
        
    
  
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  Date deposited: 26 Feb 2008
  Last modified: 08 Jan 2022 13:01
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      Contributors
      
          
          Author:
          
            
            
              V. Jurdic
            
          
        
      
          
          Author:
          
            
            
              A. Moreau
            
          
        
      
        
      
          
          Author:
          
            
            
              L.J. Enghardt
            
          
        
      
          
          Author:
          
            
            
              J. Coupland
            
          
        
      
      
      
    
  
   
  
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