A Numerical Simulation of the Inviscid Flow Through a Counterrotating Propeller

dc.contributor.author	M. L. Celestina
dc.contributor.author	J. J. Adamczyk
dc.contributor.author	R. A. Mulac
dc.date.accessioned	2017-05-08T23:23:39Z
dc.date.available	2017-05-08T23:23:39Z
dc.date.copyright	October, 1986
dc.date.issued	1986
dc.identifier.issn	0889-504X
dc.identifier.other	JOTUEI-28578#187_1.pdf
dc.identifier.uri	http://yetl.yabesh.ir/yetl/handle/yetl/101826
dc.description.abstract	This 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.
dc.publisher	The American Society of Mechanical Engineers (ASME)
dc.title	A Numerical Simulation of the Inviscid Flow Through a Counterrotating Propeller
dc.type	Journal Paper
dc.journal.volume	108
dc.journal.issue	2
dc.journal.title	Journal of Turbomachinery
dc.identifier.doi	10.1115/1.3262036
dc.journal.fristpage	187
dc.journal.lastpage	193
dc.identifier.eissn	1528-8900
dc.tree	Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 002
dc.contenttype	Fulltext