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contributor authorA. M. Yocum
contributor authorR. E. Henderson
date accessioned2017-05-08T23:08:48Z
date available2017-05-08T23:08:48Z
date copyrightJanuary, 1980
date issued1980
identifier issn1528-8919
identifier otherJETPEZ-26754#178_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/93336
description abstractA study of the effects of rotor-blade geometry, steady loading, and distortion wavelength on the distortion flow field upstream and downstream of an unstalled isolated rotor shows that the attenuation of the distortion as it passes through the rotor is a function of the blade stagger angle and the distortion-reduced frequency or the ratio of rotor blade spacing to the distortion wavelength s/l . Maximum attenuation occurs when s/l = 0.5 and increases with increasing stagger angle. Little influence of rotor incidence angle or steady loading was observed.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Effects of Some Design Parameters of an Isolated Rotor on Inlet Flow Distortions
typeJournal Paper
journal volume102
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3230219
journal fristpage178
journal lastpage186
identifier eissn0742-4795
keywordsDesign
keywordsRotors
keywordsFlow (Dynamics)
keywordsBlades
keywordsWavelength AND Geometry
treeJournal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 001
contenttypeFulltext


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