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contributor authorYang, B.
contributor authorGu, Ch. G.
date accessioned2017-05-09T01:03:26Z
date available2017-05-09T01:03:26Z
date issued2013
identifier issn0889-504X
identifier otherturb_135_1_011039.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153403
description abstractIn this study, experiments and numerical simulations were carried out to evaluate the effects of radially distorted incident flow on the performance of axialflow fans, which were equipped with three kinds of forwardskewed blades. Loss coefficient and velocity components at exit section as well as overall performance are discussed, both at the design point and the lower mass flow rate point. Furthermore, rotating stall was also observed by use of three dynamic pressure sensors. All results reveal that there are beneficial effects of forwardskewed blades on the fan performance, but the fan performance and its unsteady aerodynamic characteristics are quite affected by the radially distorted incident flow.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Effects of Radially Distorted Incident Flow on Performance of Axial Flow Fans With Forward Skewed Blades
typeJournal Paper
journal volume135
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4006535
journal fristpage11039
journal lastpage11039
identifier eissn1528-8900
treeJournal of Turbomachinery:;2013:;volume( 135 ):;issue: 001
contenttypeFulltext


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