Reducing rotor secondary losses in a turbine stage through endwall airfoil profiling
Sign Up to like & getrecommendations! Published in 2020 at "Journal of Mechanical Science and Technology"
DOI: 10.1007/s12206-020-2104-1
Abstract: The rotor blade of an experiment turbine for low Reynolds number flow conditions is recontoured on the hub endwall to reduce the hub’s secondary flow losses. The baseline rotor blade is radially stacked with airfoils… read more here.
Keywords: rotor secondary; secondary losses; hub; rotor ... See more keywords