Please use this identifier to cite or link to this item:
|Title:||Wake-structure formation of a heaving two-dimensional elliptic airfoil|
|Authors:||Lua, K.B. |
|Citation:||Lua, K.B., Lim, T.T., Yeo, K.S., Oo, G.Y. (2007-07). Wake-structure formation of a heaving two-dimensional elliptic airfoil. AIAA Journal 45 (7) : 1571-1583. ScholarBank@NUS Repository. https://doi.org/10.2514/1.25310|
|Abstract:||This paper is prompted by a recent numerical study (Lewin, G. C., and Haj-Hariri, H., "Modelling Thrust Generation of a Two-Dimensional Heaving Airfoil in Viscous Flow,"Journal of Fluid Mechanics, Vol. 492, Oct 2003, pp. 339-362) that shows that for a two-dimensional (2-D) elliptic airfoil undergoing prescribed heaving motion in a viscous fluid, both leading-edge vortices and trailing-edge vortices contributed to the formation of the wake structures. However, an earlier dye-visualization study (Lai, J. C. S., and Platzer, M. F., "Jet Characteristics of a Plunging Airfoil," AIAA Journal, Vol. 37, No. 12, 1999, pp. 1529-1537) on a heaving NACA 0012 airfoil appears to show that the wake structures were derived from trailing-edge vortices only. The dissimilarity in the two studies remains unclear because there is no corresponding experimental data on a 2-D heaving elliptic airfoil. In this study, digital particle image velocimetry technique was used to investigate the wake-structure formation of a 2-D elliptic airfoil undergoing simple harmonic heaving motion. For the range of flow conditions investigated here, our results show that the type of wake structures produced is controlled by when and how the leading-edge vortices interact with the trailing-edge vortices. Copyright © 2007 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.|
|Source Title:||AIAA Journal|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on May 18, 2018
WEB OF SCIENCETM
checked on Mar 26, 2018
checked on Apr 21, 2018
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.