A BEM for the Prediction of Unsteady Midchord Face and/or Back Propeller Cavitation

dc.contributor.author	Yin L. Young
dc.contributor.author	Doctoral Graduate Student
dc.contributor.author	Spyros A. Kinnas
dc.date.accessioned	2017-05-09T00:05:14Z
dc.date.available	2017-05-09T00:05:14Z
dc.date.copyright	June, 2001
dc.date.issued	2001
dc.identifier.issn	0098-2202
dc.identifier.other	JFEGA4-27162#311_1.pdf
dc.identifier.uri	http://yetl.yabesh.ir/yetl/handle/yetl/125435
dc.description.abstract	A boundary element method (BEM) is used for the numerical analysis of sheet cavitation on a propeller subjected to the non-axisymmetric wakes of marine vehicles. This method is extended in order to treat mixed partial and supercavity patterns on both the face and back of the blades with searched cavity detachment. The convergence of the method is studied. The predicted cavity shapes and forces by the present method agree well with experiments and with those predicted by another numerical method.
dc.publisher	The American Society of Mechanical Engineers (ASME)
dc.title	A BEM for the Prediction of Unsteady Midchord Face and/or Back Propeller Cavitation
dc.type	Journal Paper
dc.journal.volume	123
dc.journal.issue	2
dc.journal.title	Journal of Fluids Engineering
dc.identifier.doi	10.1115/1.1363611
dc.journal.fristpage	311
dc.journal.lastpage	319
dc.identifier.eissn	1528-901X
dc.keywords	Cavitation
dc.keywords	Wakes
dc.keywords	Blades
dc.keywords	Cavities
dc.keywords	Propellers AND Boundary element methods
dc.tree	Journal of Fluids Engineering:;2001:;volume( 123 ):;issue: 002
dc.contenttype	Fulltext