measure flow characteristics at high-Reynolds number flow in turbine test facility. The test
rig" TS-2" at The Central Institute of Aviation Motors was operated at the pressure up to 2.5
bar, temperature 450 C and flow rates up to 36 kg/s. The main goal of the study was to
characterize turbulence intensity and to estimate turbulence integral scale using correlation
functions in a test rig immediately before the low pressure aviation turbine. It was found that …