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contributor authorR. Mani
contributor authorA. J. Acosta
date accessioned2017-05-09T00:06:14Z
date available2017-05-09T00:06:14Z
date copyrightApril, 1968
date issued1968
identifier issn1528-8919
identifier otherJETPEZ-26668#119_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126012
description abstractA thin airfoil theory is developed for airfoils spanning a slowly diverging or converging channel, the motivation being to predict, theoretically, the effect of varying axial velocity on the cascade performance of axial flow compressor rows.
publisherThe American Society of Mechanical Engineers (ASME)
titleQuasi Two-Dimensional Flows Through a Cascade
typeJournal Paper
journal volume90
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3609146
journal fristpage119
journal lastpage127
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsCascades (Fluid dynamics)
keywordsAirfoils
keywordsAxial flow AND Channels (Hydraulic engineering)
treeJournal of Engineering for Gas Turbines and Power:;1968:;volume( 090 ):;issue: 002
contenttypeFulltext


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