Abstract
An analysis of published experimental results on the unsteady aerodynamics of separated e ow has established that the importance of the moving-wall effect is not limited to two-dimensional dynamic airfoil stall. It plays an equally prominent role in the case of three-dimensional unsteady separated e ow on a maneuvering combat aircraft. The moving-wall effect can remain effective in the presence of e ow unsteadiness. However, when the e ow unsteadiness causes bifurcation of the time-averaged e ow, the moving-wall effect can be suppressed.
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.
