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contributor authorL. H. Smith
date accessioned2017-05-08T23:26:00Z
date available2017-05-08T23:26:00Z
date copyrightJuly, 1987
date issued1987
identifier issn0889-504X
identifier otherJOTUEI-28585#313_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103207
description abstractA method being used to design unducted fans, which are counterrotating propellers with unusually high disk loadings, is described. The quasi-three-dimensional approach employed is similar to that used for ducted fan designs; it consists of a circumferential-average flowfield analysis followed by cascade designs that include secondary flow and sweep effects. The open-tip condition enters as a significant secondary flow contribution. Blade shapes defined by this process are analyzed by a three-dimensional Euler solver and final adjustments are made as necessary. Examples of application of the method are presented to elucidate the magnitudes of the phenomena involved.
publisherThe American Society of Mechanical Engineers (ASME)
titleUnducted Fan Aerodynamic Design
typeJournal Paper
journal volume109
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.3262108
journal fristpage313
journal lastpage324
identifier eissn1528-8900
keywordsDesign
keywordsFlow (Dynamics)
keywordsCascades (Fluid dynamics)
keywordsFans
keywordsDisks
keywordsBlades
keywordsPropellers AND Shapes
treeJournal of Turbomachinery:;1987:;volume( 109 ):;issue: 003
contenttypeFulltext


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