Investigation of Nonaxisymmetric Endwall Contouring and Three Dimensional Airfoil Design in a 1.5 Stage Axial Turbine—Part II: Experimental Validation

Abstract

This paper is the second part of a twopart paper reporting on the increase in efficiency of a 1.5 stage axial test rig turbine with the use of nonaxisymmetric endwalls and 3D airfoil design. Contoured endwalls were developed for the inlet guide vane separately, as well as in combination with a bowed radial profile stacking. In addition, a contour endwall was applied to the hub of the unshrouded rotor. In Part I, the design of the profiled endwalls and 3D airfoils is presented, as well as a detailed analysis of the steady and unsteady computational fluid dynamics (CFD) results. Part II reports on the experimental validation of the numerical results. A distinct increase in mechanical efficiency for both new configurations in good agreement with the numerical results is observed. Additionally, performance map measurements demonstrate that the new designs are also beneficial under offdesign conditions. Fiveand threeholeprobes as well as fastresponse total pressure probes are used to investigate the new designs. The main effect is the homogenization of the yaw angle behind the first stator.