Calculations of Wind Turbine Flow in Yaw using the BEM Technique

The earlier EU-sponsored project MEXICO (model experiments in controlled conditions) provided a huge database for flows past an experimental rotor in standard and yaw conditions. This study aims to determine the eligibility of different models under various conditions by using the MEXICO data. The m...

Full description

Bibliographic Details
Main Author: Askin, Muharrem Kemal
Format: Others
Language:English
Published: KTH, Kraft- och värmeteknologi 2011
Subjects:
BEM
CFD
Online Access:http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-187371
id ndltd-UPSALLA1-oai-DiVA.org-kth-187371
record_format oai_dc
spelling ndltd-UPSALLA1-oai-DiVA.org-kth-1873712016-08-13T05:04:30ZCalculations of Wind Turbine Flow in Yaw using the BEM TechniqueengAskin, Muharrem KemalKTH, Kraft- och värmeteknologi2011Yaw ModelGlauert’s ModelAL/NS ModelBEMCFDinduction factortip loss correctionThe earlier EU-sponsored project MEXICO (model experiments in controlled conditions) provided a huge database for flows past an experimental rotor in standard and yaw conditions. This study aims to determine the eligibility of different models under various conditions by using the MEXICO data. The main purpose of this project is to improve the BEM technique for yawed flows by using the new yaw model. Additionally, the BEM technique with new yaw model is compared with the CFD and measurement results. The Glauert’s yaw model is also applied in BEM model to compare the effectiveness of the new yaw model. It is proved that the CFD technique is still better than the BEM technique except at the high yaw and wind conditions. Furthermore, new yaw model is favored against Glauert’s yaw model. This project also aims to implement the new tip loss correction model in the BEM code and the results are validated with the CFD results. Student thesisinfo:eu-repo/semantics/bachelorThesistexthttp://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-187371application/pdfinfo:eu-repo/semantics/openAccess
collection NDLTD
language English
format Others
sources NDLTD
topic Yaw Model
Glauert’s Model
AL/NS Model
BEM
CFD
induction factor
tip loss correction
spellingShingle Yaw Model
Glauert’s Model
AL/NS Model
BEM
CFD
induction factor
tip loss correction
Askin, Muharrem Kemal
Calculations of Wind Turbine Flow in Yaw using the BEM Technique
description The earlier EU-sponsored project MEXICO (model experiments in controlled conditions) provided a huge database for flows past an experimental rotor in standard and yaw conditions. This study aims to determine the eligibility of different models under various conditions by using the MEXICO data. The main purpose of this project is to improve the BEM technique for yawed flows by using the new yaw model. Additionally, the BEM technique with new yaw model is compared with the CFD and measurement results. The Glauert’s yaw model is also applied in BEM model to compare the effectiveness of the new yaw model. It is proved that the CFD technique is still better than the BEM technique except at the high yaw and wind conditions. Furthermore, new yaw model is favored against Glauert’s yaw model. This project also aims to implement the new tip loss correction model in the BEM code and the results are validated with the CFD results.
author Askin, Muharrem Kemal
author_facet Askin, Muharrem Kemal
author_sort Askin, Muharrem Kemal
title Calculations of Wind Turbine Flow in Yaw using the BEM Technique
title_short Calculations of Wind Turbine Flow in Yaw using the BEM Technique
title_full Calculations of Wind Turbine Flow in Yaw using the BEM Technique
title_fullStr Calculations of Wind Turbine Flow in Yaw using the BEM Technique
title_full_unstemmed Calculations of Wind Turbine Flow in Yaw using the BEM Technique
title_sort calculations of wind turbine flow in yaw using the bem technique
publisher KTH, Kraft- och värmeteknologi
publishDate 2011
url http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-187371
work_keys_str_mv AT askinmuharremkemal calculationsofwindturbineflowinyawusingthebemtechnique
_version_ 1718375202701705216