Investigation of separation mechanism for airfoil leading edge flow at low Reynolds number
JOURNAL- BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS ; 30 , 8 ; 693-697
2004-01-01
5 pages
Article (Journal)
Unknown
DDC: | 629.4 |
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Aerodynamic Control of Low-Reynolds-Number Airfoil with Leading-Edge Protuberances
Online Contents | 2013
|