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RISDiscussion: “Effects of Tip Clearance on Blade Loading in a Planar Cascade of Turbine Blades” (Sjolander, S. A., and Amrud, K. K., 1987, ASME J. Turbomach., 109, pp. 237–244)
Publisher: The American Society of Mechanical Engineers (ASME)
Annular Cascade Testing of Turbine Nozzles at High Exit Mach Numbers
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper presents detailed information on the three-dimensional flow field in a realistic low aspect ratio, high turning nozzle vane design which incorporates end-wall contouring and which has ...
The Effect of a Downstream Rotor on the Measured Performance of a Transonic Turbine Nozzle
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Two nozzle designs, involving the same low aspect ratio, high turning angle vanes, and differing in outer wall contour, were tested over a range of exit Mach numbers up to supersonic values. ...
Influence of Rotor Blade Aerodynamic Loading on the Performance of a Highly Loaded Turbine Stage
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper describes the performance of a highly loaded single-stage transonic turbine with a pressure ratio of 3.76 and a stage loading factor of 2.47. Tests were carried out with three ...
An Experimental Assessment of the Influence of Downstream Conditions on the Performance of a Transonic Turbine Nozzle of High Turning
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The present work was conducted to extend information derived in a previous study where it was found that the performance of a transonic turbine nozzle of high turning angle was significantly ...