“…While analyzing experimental data, it should be mentioned that the greatest influence on the nozzle efficiency is exerted by geometrical expansion angle of supersonic nozzle of jet reaction turbine γ, this is indicated by the coefficients of appropriate variables in regression equation. The obtained results agree with the data of other researchers [16,17,18,19,20,21] and provide additional information. Herewith, the experimental point 6 provides the greatest efficiency of pneumatic two-stage small-size radial turbine.…”