Influence of propeller overlap on large-scale tandem UAV performance
Influence of propeller overlap on large-scale tandem UAV performance
  This paper investigates the interference that arises from overlapping Unmanned Aerial Vehicle (UAV) propellers during hovering flight. The tests have been conducted on 28” x  8.4” ultralight carbon fiber propellers using a bespoke mount and the RCBenchmark Series 1780 dynamometer at various degrees of overlap (d / D) and vertical separation (z / D). A great deal of confusion regarding the losses that are associated with mounting propellers in a co-axial configuration is reported in the literature, with a summary of historical tandem helicopters having been conducted. The results highlight a region of beneficial overlap (0–20%), which has the potential to be advantageous to a wide range of UAVs.
  Rotor Losses, overlapping, Drone, Multi-rotor, Unmanned, Aircraft, Optimization, propeller, tandem
  
  
  245-260
  
    
      Weishaupl, Adrian B.
      
        89f47b12-9afb-482a-ab61-163ef9685211
      
     
  
    
      Prior, Stephen D.
      
        9c753e49-092a-4dc5-b4cd-6d5ff77e9ced
      
     
  
  
   
  
  
    
    
  
    
      3 September 2019
    
    
  
  
    
      Weishaupl, Adrian B.
      
        89f47b12-9afb-482a-ab61-163ef9685211
      
     
  
    
      Prior, Stephen D.
      
        9c753e49-092a-4dc5-b4cd-6d5ff77e9ced
      
     
  
       
    
 
  
    
      
  
  
  
  
  
  
    Weishaupl, Adrian B. and Prior, Stephen D.
  
  
  
  
   
    (2019)
  
  
    
    Influence of propeller overlap on large-scale tandem UAV performance.
  
  
  
  
    Unmanned Systems, 7 (4), .
  
   (doi:10.1142/S2301385019500092). 
  
  
   
  
  
  
  
  
   
  
    
    
      
        
          Abstract
          This paper investigates the interference that arises from overlapping Unmanned Aerial Vehicle (UAV) propellers during hovering flight. The tests have been conducted on 28” x  8.4” ultralight carbon fiber propellers using a bespoke mount and the RCBenchmark Series 1780 dynamometer at various degrees of overlap (d / D) and vertical separation (z / D). A great deal of confusion regarding the losses that are associated with mounting propellers in a co-axial configuration is reported in the literature, with a summary of historical tandem helicopters having been conducted. The results highlight a region of beneficial overlap (0–20%), which has the potential to be advantageous to a wide range of UAVs.
         
      
      
        
          
            
  
    Text
 US Journal Submission 2 V4
     - Accepted Manuscript
   
  
  
    
  
 
          
            
          
            
           
            
           
        
          
        
        
       
    
   
  
  
  More information
  
    
      Accepted/In Press date: 14 May 2019
 
    
      Published date: 3 September 2019
 
    
  
  
    
  
    
  
    
  
    
  
    
  
    
     
        Keywords:
        Rotor Losses, overlapping, Drone, Multi-rotor, Unmanned, Aircraft, Optimization, propeller, tandem
      
    
  
    
  
    
  
  
  
    
  
  
        Identifiers
        Local EPrints ID: 433170
        URI: http://eprints.soton.ac.uk/id/eprint/433170
        
          
        
        
        
          ISSN: 2301-3850
        
        
          PURE UUID: 6a251dd7-2feb-40f8-8379-377b893926ec
        
  
    
        
          
        
    
        
          
            
              
            
          
        
    
  
  Catalogue record
  Date deposited: 09 Aug 2019 16:30
  Last modified: 06 Jun 2024 04:09
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      Contributors
      
          
          Author:
          
            
            
              Adrian B. Weishaupl
            
          
        
      
        
      
      
      
    
  
   
  
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