Abstract
Abstract
With use, new turbine blades experience a change in profile and surface roughness. An experimental study has been carried out in rectilinear cascades of reaction and impulse blades with smooth and rough surfaces. The roughnesses of 220, 100, and 50 grades emery paper, one at a time, is applied over suction and pressure surfaces at one-third of surface at leading edge, mid-chord and trailing edge regions. Measurement of pressure, exit angle, and velocity at exit of the cascade has been taken with a three-hole probe. It has been observed that the same roughness at mid-chord of suction surface is most detrimental and least detrimental when applied at mid-chord of pressure surface. It has also been seen that the same roughness over impulse blade is more detrimental than that over reaction blade.
Keywords
Get full access to this article
View all access options for this article.
