ATTENTION: The software behind KU ScholarWorks is being upgraded to a new version. Starting July 15th, users will not be able to log in to the system, add items, nor make any changes until the new version is in place at the end of July. Searching for articles and opening files will continue to work while the system is being updated.
If you have any questions, please contact Marianne Reed at mreed@ku.edu .
The effect of variations in first- and second-order derivatives on airfoil aerodynamic performance
dc.contributor.author | Yi, Penghui | |
dc.contributor.author | Wang, Ying | |
dc.contributor.author | Sun, Xiaojing | |
dc.contributor.author | Huang, Diangui | |
dc.contributor.author | Zheng, Zhongquan | |
dc.date.accessioned | 2018-12-14T18:50:37Z | |
dc.date.available | 2018-12-14T18:50:37Z | |
dc.date.issued | 2016-12-04 | |
dc.identifier.citation | Penghui Yi, Ying Wang, Xiaojing Sun, Diangui Huang & Zhongquan Zheng (2017) The effect of variations in first- and second-order derivatives on airfoil aerodynamic performance, Engineering Applications of Computational Fluid Mechanics, 11:1, 54-68, DOI: 10.1080/19942060.2016.1246264 | en_US |
dc.identifier.uri | http://hdl.handle.net/1808/27515 | |
dc.description.abstract | The geometric factors which influence airfoil aerodynamic performance are attributed to variations in local first- and second-order curvature derivatives. Based on a self-developed computational fluid dynamics (CFD) program called UCFD, the influence of local profile variations on airfoil aerodynamic performance in different pressure areas is investigated. The results show that variations in first- and second-order derivatives of the airfoil profiles can cause fluctuations in airfoil aerodynamic performance. The greater the variation in local first- and second-order derivatives, the greater the fluctuation amplitude of the airfoil aerodynamic coefficients. Moreover, at the area near the leading edge and the shock-wave position, the surface pressure is more sensitive to changes in first- and second-order derivatives. These results provide a reference for airfoil aerodynamic shape design. | en_US |
dc.publisher | Taylor & Francis | en_US |
dc.rights | © 2016 The Author(s). Published by Informa UK Limited, trading as Taylor & Francis Group. This is an Open Access article distributed under the terms of the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited | en_US |
dc.rights.uri | https://creativecommons.org/licenses/by/4.0/ | en_US |
dc.subject | Geometric airfoil profile | en_US |
dc.subject | Derivative | en_US |
dc.subject | Variation | en_US |
dc.subject | Surface pressure coefficient | en_US |
dc.title | The effect of variations in first- and second-order derivatives on airfoil aerodynamic performance | en_US |
dc.type | Article | en_US |
kusw.kuauthor | Zheng, Zhongquan | |
kusw.kudepartment | Aerospace Engineering | en_US |
dc.identifier.doi | 10.1080/19942060.2016.1246264 | en_US |
kusw.oaversion | Scholarly/refereed, publisher version | en_US |
kusw.oapolicy | This item meets KU Open Access policy criteria. | en_US |
dc.rights.accessrights | openAccess | en_US |
Files in this item
This item appears in the following Collection(s)
Except where otherwise noted, this item's license is described as: © 2016 The Author(s). Published by Informa UK Limited, trading as Taylor & Francis Group. This is an Open Access article distributed under the terms of the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited