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contributor authorMarco Raciti Castelli
contributor authorErnesto Benini
date accessioned2017-05-09T00:55:19Z
date available2017-05-09T00:55:19Z
date copyrightMay, 2012
date issued2012
identifier issn0889-504X
identifier otherJOTUEI-28785#031016_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/150524
description abstractThis paper presents a model for the evaluation of energy performance and aerodynamic forces acting on a small helical Darrieus vertical axis wind turbine depending on blade inclination angle. It consists of an analytical code coupled to a solid modeling software capable of generating the desired blade geometry depending on the desired design geometric parameters, which is linked to a finite volume CFD code for the calculation of rotor performance. After describing and validating the model with experimental data, the results of numerical simulations are proposed on the bases of five machine architectures, which are characterized by an inclination of the blades with respect to the horizontal plane in order to generate a phase shift angle between lower and upper blade sections of 0 deg, 30 deg, 60 deg, 90 deg, and 120 deg for a rotor having an aspect ratio of 1.5. The effects of blade inclination on tangential and axial forces are first discussed and then the overall rotor torque is considered as a function of azimuthal position of the blades. Finally, the downstream tip recirculation zone due to the finite blade extension is analyzed for each blade inclination angle, achieving a numerical quantification of the influence of induced drag on rotor performance, as a function of both blade element longitudinal and azimuthal positions of the blade itself.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffect of Blade Inclination Angle on a Darrieus Wind Turbine
typeJournal Paper
journal volume134
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4003212
journal fristpage31016
identifier eissn1528-8900
keywordsRotors
keywordsBlades AND Torque
treeJournal of Turbomachinery:;2012:;volume( 134 ):;issue: 003
contenttypeFulltext


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