30th Congress of the International Council of the Aeronautical Sciences

04 - Propulsion

EFFECT OF REYNOLDS NUMBER, OPERATING MODE, TURBULENCE PARAMETERS ON PROFILE AND SECONDARY LOSSES OF LPT

A.D. Nepomnyashchiy¹, S.V. Suntsov ¹, S.Y. Danilkin¹, V.P. Maslov¹; ¹Central Institute of Aviation Motors (CIAM), Russia

Two flat turbine cascades have been experimentally investigated in a wide range of the reduced isentropic velocity and the Reynolds number under various turbulent parameters of a flow at the cascades’ inlet generated by means of grids. Turbulence parameters were measured using a hot-wire anemometer and a high-frequency pressure probe.


View Paper