Modeling of Pitching and Plunging Airfoils at Reynolds Number between 1x10^4 and 6x10^4
27th, AIAA Applied Aerodynamics Conference ; 2009 ; San Antonio, TX
01.01.2009
23 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
| British Library Conference Proceedings | 2009
Experimental study of pitching and plunging airfoils at low Reynolds numbers
| Tema Archiv | 2012
Fluid Dynamics of Pitching and Plunging Airfoils of Reynolds Number between 1x10^4 and 6x10^4
| British Library Conference Proceedings | 2009