Abstract
The aerodynamic characteristics of rectangular, elliptical and triangular planforms with an aspect ratio of 4 are investigated at low Reynolds number regime (Re = 60,000 5,000) in a low density wind tunnel. This paper describes the effects of Reynolds number and the planeforms on the aerodynamic performance for each wing. The aerodynamic performance is little affected by Reynolds number effects, however a change of the stall characteristics and an increase of the drag coefficient are observed at Re = 5,000. Compared with the aerodynamic characteristics for each planform at the same Reynolds number, there is a remarkable difference in the stall characteristics.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.