Please use this identifier to cite or link to this item:
|Title:||On the prolong attachment of leading edge vortex on a flapping wing||Authors:||Lim, T.T.
|Keywords:||Leading edge vortex
|Issue Date:||30-Jan-2009||Citation:||Lim, T.T., Teo, C.J., Lua, K.B., Yeo, K.S. (2009-01-30). On the prolong attachment of leading edge vortex on a flapping wing. Modern Physics Letters B 23 (3) : 357-360. ScholarBank@NUS Repository. https://doi.org/10.1142/S0217984909018394||Abstract:||In this paper, we take a fundamental approach to investigate the effect of spanwise flow on the prolonged attachment of leading edge vortex (LEV) on a flapping wing. By imposing a constant acceleration-constant velocity flow on elliptic wings of various sweep angles and angles of attack, our experimental and numerical results show that while spanwise flow per se has negligible influence on the prolong attachment of the LEV, vortex stretching can significantly delay detachment of the LEV, even for a small spanwise flow. © 2009 World Scientific Publishing Company.||Source Title:||Modern Physics Letters B||URI:||http://scholarbank.nus.edu.sg/handle/10635/73715||ISSN:||02179849||DOI:||10.1142/S0217984909018394|
|Appears in Collections:||Staff Publications|
Show full item record
Files in This Item:
There are no files associated with this item.
checked on Oct 14, 2019
WEB OF SCIENCETM
checked on Oct 7, 2019
checked on Oct 13, 2019
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.