Title:
Numerical investigation on the use of multi-element blades in vertical-axis wind turbines

dc.contributor.advisor Sankar, Lakshmi N.
dc.contributor.advisor Jagoda, Jechiel I.
dc.contributor.author Bah, Elhadji Alpha Amadou
dc.contributor.committeeMember Costello, Mark
dc.contributor.committeeMember Schrage, Daniel
dc.contributor.committeeMember Shelton, Samuel
dc.contributor.department Aerospace Engineering
dc.date.accessioned 2015-06-08T18:20:41Z
dc.date.available 2015-06-08T18:20:41Z
dc.date.created 2015-05
dc.date.issued 2015-01-12
dc.date.submitted May 2015
dc.date.updated 2015-06-08T18:20:41Z
dc.description.abstract The interest in sustainable forms of energy is being driven by the anticipated scarcity of traditional fossil fuels over the coming decades. There is also a growing concern about the effects of fossil fuel emissions on human health and the environment. Many sources of renewable energy are being researched and implemented for power production. In particular, wind power generation by horizontal- and vertical-axis wind turbines is very popular. Vertical-axis wind turbines (VAWTs) have a relative construction simplicity compared to horizontal-axis wind turbines (HAWTs). However, VAWTs present specific challenges that may hinder their performance. For instance, they are strongly affected by dynamic stall. A significant part of the kinetic energy contained in the oncoming wind is lost in swirl and vortices. As a result, VAWTs have lower power production compared to HAWTs. First, the present work is aimed at the study of the aerodynamics of straight-bladed VAWTs (SB-VAWTs). Empirical calculations are conducted in a preliminary work. Then a two-dimensional double multiple streamtube (DMST) approach supported by a two-dimensional numerical study is implemented. The dynamic stall and aerodynamic performance of the rotor are investigated. A VAWT-fitted dynamic stall model is implemented. Computational fluid dynamics (CFD) simulations are conducted to serve as reference for the DMST calculations. This three-pronged approach allows us to efficiently explore multiple configurations. The dynamic stall phenomenon is identified as a primary cause of performance loss. The results in this section validate the DMST model as a good replacement for CFD analysis in early phase design provided that a good dynamic stall model is used. After having identify the primary cause of performance loss, the goal is to investigate the use to dual-element blades for alleviating the effect of dynamic stall, thereby improving the performance of the rotor. The desirable airfoil characteristics are defined and a parametric analysis conducted. In the present study the parameters consists of the size of the blade elements, the space between them, and their relative orientation. The performance of the rotor is calculated and compared to the baseline. The results highlight the preeminence of the two-element configuration over the single-element provided that the adequate parametric study is conducted beforehand. A performance enhancement is obtained over a large range of tip speed ratios. The starting characteristics and the operation stability are also improved. Finally, an economic analysis is conducted to determine the cost of energy and thus the financial viability of such a project. The Great Coast of Senegal is selected as site of operation. The energy need and sources of this region are presented along with its wind energy potential. The cost evaluation shows the economic viability by comparing the cost of energy to the current energy market prices.
dc.description.degree Ph.D.
dc.format.mimetype application/pdf
dc.identifier.uri http://hdl.handle.net/1853/53501
dc.language.iso en_US
dc.publisher Georgia Institute of Technology
dc.subject CFD
dc.subject VAWT
dc.subject DMST
dc.subject Dynamic stall
dc.subject Multi-elements
dc.subject Financial viability
dc.title Numerical investigation on the use of multi-element blades in vertical-axis wind turbines
dc.type Text
dc.type.genre Dissertation
dspace.entity.type Publication
local.contributor.advisor Sankar, Lakshmi N.
local.contributor.advisor Jagoda, Jechiel I.
local.contributor.corporatename College of Engineering
local.contributor.corporatename Daniel Guggenheim School of Aerospace Engineering
local.relation.ispartofseries Doctor of Philosophy with a Major in Aerospace Engineering
relation.isAdvisorOfPublication 22a68276-4f0c-499c-9dd9-931e34bf40a8
relation.isAdvisorOfPublication 82d8814b-a147-40a3-908d-cb7a4766cdbe
relation.isOrgUnitOfPublication 7c022d60-21d5-497c-b552-95e489a06569
relation.isOrgUnitOfPublication a348b767-ea7e-4789-af1f-1f1d5925fb65
relation.isSeriesOfPublication f6a932db-1cde-43b5-bcab-bf573da55ed6
thesis.degree.level Doctoral
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