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contributor authorBalduzzi, Francesco
contributor authorBianchini, Alessandro
contributor authorMaleci, Riccardo
contributor authorFerrara, Giovanni
contributor authorFerrari, Lorenzo
date accessioned2017-05-09T01:24:20Z
date available2017-05-09T01:24:20Z
date issued2015
identifier issn0889-504X
identifier otherturbo_137_01_011006.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/159874
description abstractDarrieus wind turbines are experiencing a renewed interest in the wind energy scenario, in particular, whenever small and mediumsize installations are considered. In these contexts, the average wind speeds are generally quite low due to scale effects and therefore the most exploited design choices for the turbines are the Hshape configuration, as the entire blade can take advantage of the maximum rotational radius, and high chord to radius ratios, in order to ensure suitable Reynolds numbers on the airfoils. By doing so, the aerodynamic effects induced by the motion of the airfoils in a curved flowpath become more evident and the airfoils themselves have to be designed to compensate these phenomena if conventional design tools based on the blade element momentum (BEM) theory are used. In this study, fully unsteady 2D simulations were exploited to analyze a threebladed HDarrieus wind turbine in order to define the real flow structure and its effects on the turbine performance; in detail, the influence of both the virtual camber and the virtual incidence were investigated. Computational fluid dynamics (CFD) results were supported by experimental data collected on fullscale models reproducing two different airfoil mountings. Finally, the proper design criteria to compensate these phenomena are proposed and their benefits on a conventional simulation with a BEM approach are discussed.
publisherThe American Society of Mechanical Engineers (ASME)
titleBlade Design Criteria to Compensate the Flow Curvature Effects in H Darrieus Wind Turbines
typeJournal Paper
journal volume137
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4028245
journal fristpage11006
journal lastpage11006
identifier eissn1528-8900
treeJournal of Turbomachinery:;2015:;volume( 137 ):;issue: 001
contenttypeFulltext


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