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contributor authorN. Venkatrayulu
contributor authorD. Prithvi Raj
contributor authorR. G. Narayanamurthi
date accessioned2017-05-08T23:08:46Z
date available2017-05-08T23:08:46Z
date copyrightJanuary, 1980
date issued1980
identifier issn1528-8919
identifier otherJETPEZ-26754#75_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/93317
description abstractThis paper presents the results of experimental investigations on the three-dimensional flow and performance characteristics of a free vortex axial flow fan rotor, with a freely rotating and braked inlet guide vane row. The influences of axial distance between the inlet guide vane row and the rotor inlet, inlet guide vane setting angle and shape, partial omission of guide vanes at the hub and tip regions on the return flows have been studied and optimum axial distance and setting angle that will improve the useful operating range of the fan were determined. Use of freely rotating inlet guide vanes at high flow volumes and braked inlet guide vanes at low flow coefficients resulted in a reduction of return flows and an increase of the stable operating range of the axial fan rotor by more than 35 percent and this combination has yielded higher efficiencies as well in the extended region of stable operation.
publisherThe American Society of Mechanical Engineers (ASME)
titleInfluence of Freely Rotating Inlet Guide Vanes on the Return Flows and Stable Operating Range of an Axial Flow Fan
typeJournal Paper
journal volume102
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3230237
journal fristpage75
journal lastpage80
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsAxial flow
keywordsRotors
keywordsVortices
keywordsShapes AND Performance characterization
treeJournal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 001
contenttypeFulltext


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