Abstract
The paper presents the results of experiments conducted in subsonic wind tunnels at low Reynolds numbers. A rough (fleecy) thread was pulled in front of the wing model at a considerable distance from it, the trace of which fell on the wing surface. We studied the flow patterns on the surface of the wing before and after exposure at various angles of attack and angles of sweep of the wing. It was found that the trail has a significant effect on the flow separation and on the vortex structures arising above the wing.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: 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.
