Parametric Design Study of the Thickness of Airfoils at Reynolds Numbers from 60,000 to 150,000
- 5 January 2004
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Micro-Air-Vehicles: Can They be Controlled Better?Journal of Aircraft, 2001
- A Computational Study on Airfoils at a Low Reynolds NumberPublished by ASME International ,2000
- Rigid and Flexible Low Reynolds Number AirfoilsJournal of Aircraft, 1999