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contributor authorN. A. Mitchell
date accessioned2017-05-08T23:11:12Z
date available2017-05-08T23:11:12Z
date copyrightJanuary, 1981
date issued1981
identifier issn1528-8919
identifier otherJETPEZ-26763#201_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94581
description abstractA three-dimensional nonaxisymmetric theory is presented to analyze the interaction effects due to wakes between two blade rows in an axial turbomachine. The relative importance of potential and wake interaction with varying row separations and the contribution to the flow of shed radial and shed streamwise vorticity from the first row are examined. Numerical calculations of turbine and compressor stages are presented to illustrate the theory.
publisherThe American Society of Mechanical Engineers (ASME)
titleNonaxisymmetric Blade Row Interaction in Axial Turbomachines
typeJournal Paper
journal volume103
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3230698
journal fristpage201
journal lastpage209
identifier eissn0742-4795
keywordsBlades
keywordsTurbomachinery
keywordsWakes
keywordsVorticity
keywordsTurbines
keywordsFlow (Dynamics) AND Compressors
treeJournal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 001
contenttypeFulltext


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