Investigation of separation mechanism for airfoil leading edge flow at low Reynolds number
JOURNAL- BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS ; 30 , 8 ; 693-697
01.01.2004
5 pages
Aufsatz (Zeitschrift)
Unbekannt
DDC: | 629.4 |
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Aerodynamic Control of Low-Reynolds-Number Airfoil with Leading-Edge Protuberances
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