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contributor authorC. M. Vaczy
contributor authorD. C. McCormick
date accessioned2017-05-08T23:26:00Z
date available2017-05-08T23:26:00Z
date copyrightJuly, 1987
date issued1987
identifier issn0889-504X
identifier otherJOTUEI-28585#325_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103208
description abstractAn oil flow visualization study was conducted on the blades of a counterrotating prop-fan model, the CRP-X1. A kink in the oil streaks was interpreted as an indication of the leading edge vortex reattachment line. The leading edge vortex was found to be on the lower surface for cases with negative leading edge loading and on the upper surface for cases with positive leading edge loading. For most cases, the leading edge vortex merged with a tip vortex. The results presented here represent the first systematic study of this phenomenon.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Study of the Leading Edge Vortex and Tip Vortex on Prop-Fan Blades
typeJournal Paper
journal volume109
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262109
journal fristpage325
journal lastpage331
identifier eissn1528-8900
keywordsWake turbulence
keywordsVortices
keywordsBlades
keywordsCarbon reinforced plastics AND Flow visualization
treeJournal of Turbomachinery:;1987:;volume( 109 ):;issue: 003
contenttypeFulltext


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