Preliminary Results of Some Experiments with a Vortex Augmented Wing

720321

02/01/1972

Event
National Business Aircraft Meeting and Engineering Display
Authors Abstract
Content
A wind tunnel investigation was made of a new high-lift system consisting of a leading edge cusp flap combined with split upper and lower trailing edge flaps. The idea behind the system was to generate two strong spanwise vortices that would increase maximum lift and drag simultaneously. Test results were not encouraging. The spanwise vortices were observed, but were not sufficiently strong to generate the anticipated high lift. Several interesting flow phenomena were observed and are described. The purpose of this paper is to present a summary of results obtained from this wind tunnel test program.
Meta TagsDetails
DOI
https://doi.org/10.4271/720321
Pages
12
Citation
Roskam, J., and Gleason, M., "Preliminary Results of Some Experiments with a Vortex Augmented Wing," SAE Technical Paper 720321, 1972, https://doi.org/10.4271/720321.
Additional Details
Publisher
Published
Feb 1, 1972
Product Code
720321
Content Type
Technical Paper
Language
English