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contributor authorM. W. Benner
contributor authorS. H. Moustapha
contributor authorS. A. Sjolander
date accessioned2017-05-08T23:55:09Z
date available2017-05-08T23:55:09Z
date copyrightApril, 1997
date issued1997
identifier issn0889-504X
identifier otherJOTUEI-28659#193_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/119625
description abstractThe most recent correlations for turbine profile losses at off-design incidence include the leading-edge diameter as the only aspect of the leading-edge geometry that influences the losses. Cascade measurements are presented for two turbine blades that differ primarily in their leading-edge geometries. The incidence was varied over a range of ±20 deg and the results show significant discrepancies between the observed profile losses and those predicted by the available correlations. Using data from the present experiments, as well as cases from the literature for which sufficient geometric data are given, a revised correlation has been developed. The new correlation is a function of both the leading-edge diameter and the wedge angle, and it is significantly more successful than the existing correlations. It is argued that the off-design loss behavior of the blade is influenced by the magnitude of the discontinuity in curvature at the points where the leading-edge circle meets the rest of the blade profile. The wedge angle appears to be an approximate and convenient measure of the discontinuity in curvature at these blend points.
publisherThe American Society of Mechanical Engineers (ASME)
titleInfluence of Leading-Edge Geometry on Profile Losses in Turbines at Off-Design Incidence: Experimental Results and an Improved Correlation
typeJournal Paper
journal volume119
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2841101
journal fristpage193
journal lastpage200
identifier eissn1528-8900
keywordsDesign
keywordsTurbines
keywordsGeometry
keywordsWedges
keywordsBlades
keywordsMeasurement
keywordsTurbine blades AND Cascades (Fluid dynamics)
treeJournal of Turbomachinery:;1997:;volume( 119 ):;issue: 002
contenttypeFulltext


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