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contributor authorM. L. Celestina
contributor authorJ. J. Adamczyk
contributor authorR. A. Mulac
date accessioned2017-05-08T23:23:39Z
date available2017-05-08T23:23:39Z
date copyrightOctober, 1986
date issued1986
identifier issn0889-504X
identifier otherJOTUEI-28578#187_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101826
description abstractThis paper presents the results of a numerical simulation of the time-averaged inviscid flow field through the blade rows of a multiblade row turboprop configuration. The governing equations are outlined along with a discussion of the solution procedure and coding strategy. Numerical results obtained from a simulation of the flow field through a modern high-speed turboprop will be shown.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Numerical Simulation of the Inviscid Flow Through a Counterrotating Propeller
typeJournal Paper
journal volume108
journal issue2
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262036
journal fristpage187
journal lastpage193
identifier eissn1528-8900
treeJournal of Turbomachinery:;1986:;volume( 108 ):;issue: 002
contenttypeFulltext


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