Experimental Investigations of Strongly Swept Turbine Cascades with low Speed Flow

Author:

Hill J. M.1,Lewis R. I.2

Affiliation:

1. Formerly at the Department of Mechanical Engineering, University of Newcastle upon Tyne

2. Professor of Fluid Mechanics and Thermodynamics, Department of Mechanical Engineering, University of Newcastle upon Tyne

Abstract

Results are presented from an investigation into the blade to blade and meridional flow perturbations arising in high deflection turbine cascades subjected to large sweep angles. Experimental work has confirmed previous analytical estimates of the effect of sweep and indicated that certain common design procedures for the calculation of blade to blade flows are seriously in error. The significance of the results with reference to practical design considerations is discussed.

Publisher

SAGE Publications

Subject

General Engineering

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Numerical research on the trailing-edge sweep of supersonic/transonic turbines;Aerospace Science and Technology;2020-04

2. Rotor Blade Sweep Effect on the Performance of a Small Axial Supersonic Impulse Turbine;International Journal of Aeronautical and Space Sciences;2015-12-30

3. Improving Intermediate Pressure Turbine Performance by Using a Nonorthogonal Stator;Journal of Turbomachinery;2013-09-26

4. Influence of Sweep on Axial Flow Turbine Aerodynamics at Midspan;Journal of Turbomachinery;2006-07-14

5. Lifting-surface theory of straight cascades of swept blades;International Journal of Mechanical Sciences;1976-06

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