The Bladeless Propeller 



3.0 



2.0 



STATIC OPERATION 



THEORY, 



■^liVzi* ' *° 



THEORY, 



Tii'/Tai* - I.O)(REF 12) 

 O EXP'T, 



Tii'/Tji* « 1.0 

 n EXP'T, 



Tii'/Tji* - 1.0 (REF. 17) 



2S< 



30« 



Fig. 14 - Effect of mixing during the 

 deflection phase 



analyzed by the strip approach, but with consideration of meridional deflections 

 of the primary jet. In addition, these analyses stipulate the presence of (a) sec- 

 ondary prerotation guidevanes for the purpose of obtaining radial uniformity of 

 energy transfer, hence radial dynamic equilibrium, (b) exit straightening vanes 

 for the purpose of turning the secondary flow, after the interaction, everywhere 

 to the axial direction, and (c) a separator for the extraction of the deflected pri- 

 mary flow, which is then also turned to the axial direction and discharged isen- 

 tropically to ambient pressure. Numerical results of these analyses, for a 



1365 



