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dc.contributorDepartment of Building Environment and Energy Engineeringen_US
dc.creatorChen, Jen_US
dc.creatorChen, Len_US
dc.creatorXu, Hen_US
dc.creatorYang, Hen_US
dc.creatorYe, Cen_US
dc.creatorLiu, Den_US
dc.date.accessioned2023-11-17T02:59:10Z-
dc.date.available2023-11-17T02:59:10Z-
dc.identifier.issn0360-5442en_US
dc.identifier.urihttp://hdl.handle.net/10397/102972-
dc.language.isoenen_US
dc.publisherPergamon Pressen_US
dc.rights© 2016 Elsevier Ltd. All rights reserved.en_US
dc.rights© 2016. This manuscript version is made available under the CC-BY-NC-ND 4.0 license https://creativecommons.org/licenses/by-nc-nd/4.0/.en_US
dc.rightsThe following publication Chen, J., Chen, L., Xu, H., Yang, H., Ye, C., & Liu, D. (2016). Performance improvement of a vertical axis wind turbine by comprehensive assessment of an airfoil family. Energy, 114, 318-331 is available at https://doi.org/10.1016/j.energy.2016.08.005.en_US
dc.subjectACFDA moduleen_US
dc.subjectAirfoil assessmenten_US
dc.subjectFlow fielden_US
dc.subjectImpact weighten_US
dc.subjectOrthogonal algorithmen_US
dc.subjectPower coefficient (CP)en_US
dc.titlePerformance improvement of a vertical axis wind turbine by comprehensive assessment of an airfoil familyen_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage318en_US
dc.identifier.epage331en_US
dc.identifier.volume114en_US
dc.identifier.doi10.1016/j.energy.2016.08.005en_US
dcterms.abstractStudies on lift-type VAWTs are far fewer than those on horizontal VAWTS, especially in the field of airfoil, which is regarded as the fundamental of VAWT design. Existing researches seldom systematically and efficiently touch upon a specific airfoil family. Thus, a coupled approach comprising two steps was used in this paper to assess an airfoil family, wherein the first step was the orthogonal algorithm combined with an automatic computational fluid dynamic analysis (ACFDA) module, and the second step was the combination of the one-factor at a time (OFAAT) algorithm and the ACFDA module.en_US
dcterms.abstractResults demonstrate that among three design parameters, the thickness-chord ratio (TCR) had the biggest effect on CP while the maximum thickness in tenths of chord (MTITOC) had the smallest influence on CP. By this approach, we found a desired airfoil having maximum power coefficient(CPMAX) was 0.4585, app. 15.5% higher than that of the previously widely used rotor NACA 0015. In addition, detailed flow data (field) dispersing in the vicinity of the airfoil were visualized to reveal the effect of each design parameter on airfoil's aerodynamic behavior. Lastly, this coupled approach can be used to assess any airfoil family that can be parameterized and has several design parameters.en_US
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationEnergy, 1 Nov. 2016, v. 114, p. 318-331en_US
dcterms.isPartOfEnergyen_US
dcterms.issued2016-11-01-
dc.identifier.scopus2-s2.0-84981308669-
dc.identifier.eissn1873-6785en_US
dc.description.validate202310 bckwen_US
dc.description.oaAccepted Manuscripten_US
dc.identifier.FolderNumberBEEE-0740-
dc.description.fundingSourceOthersen_US
dc.description.fundingTextShanghai Pujiang Program; Shanghai Outstanding Talents Support Program; The Hong Kong Polytechnic Universityen_US
dc.description.pubStatusPublisheden_US
dc.identifier.OPUS6666295-
dc.description.oaCategoryGreen (AAM)en_US
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