Exploring the effects of spanwise wing deformation on lift coefficient and trailing vortices properties at low Reynolds number.
Loading...
Files
Description: Abstract
Identifiers
Publication date
Reading date
Collaborators
Advisors
Tutors
Editors
Journal Title
Journal ISSN
Volume Title
Publisher
Share
Department/Institute
Keywords
Abstract
We have conducted an experimental investigation on the effect of spanwise wing deformation on the lift coefficient and the properties of the wingtip vortices generated by several NACA0012 symmetric wing models.