ReseArch and optimising of preswirl in radial-axial inlet
Project full name:
Research and optimising of preswirl in radial-axial inlet with regard to design parameter attaining and mutual cooperation with first stages of the axial flow compressor of small turbine engine
Project objectives:
Research of cooperation between radial-axial inlet and mixed (axial + centrifugal) compressor. Efficiency optimisation, manufacture of experimental parts - verification of designed parameters.
Project participants: