Incidence Angle and Pitch–Chord Effects on Secondary Flows Downstream of a Turbine Cascade

TLDR: In this paper, the results of an experimental investigation of the three-dimensional flow downstream of a linear turbine cascade at off-design conditions are described. But the results are limited to five incidence angles from − 60 to + 35 deg, and for three pitch-chord ratios: s/c = 0.58, 0.73, and 0.87.

Abstract: This paper describes the results of an experimental investigation of the three-dimensional flow downstream of a linear turbine cascade at off-design conditions. The tests have been carried out for five incidence angles from − 60 to + 35 deg, and for three pitch-chord ratios: s/c = 0.58, 0.73, 0.87. Data include blade pressure distributions, oil flow visualizations, and pressure probe measurements. The secondary flow field has been obtained by traversing a miniature five-hole probe in a plane located at 50 percent of an axial chord downstream of the trailing edge. The distributions of local energy loss coefficients, together with vorticity and secondary velocity plots, show in detail how much the secondary flow field is modified both by incidence and by cascade solidity variations