Aerospace & Aeronautical Engineering

Aerothermodynamics

The aerothermodynamics performance of a binary- entry radial turbine has been assessed, and the maximum effectiveness is shown to do when the mass inflow at the cloak side of volute is further than mecca side. The influence of the lingo wake is depicted by a low instigation toward the rotor entry, but the effect of this critical region doesn't extend beyond a tangential angle of 90 deg. Also, the interspace region is characterized by inflow mixing between the inflow at exit of cloak side and mecca side of volute.