Abstract
To predict the full-scale aerodynamics of a combat aircraft performing high-alpha maneuvers requires the combined usage of experimental and theoretical tools. The preferred experimental tool is the rotary rig because it provides simulation of one important component of advanced maneuvers, i.e., the velocity vector roll. The present paper analyzes the results obtained in the recently completed investigation by AGARD FDP Working Group 16. Anomalous results are obtained when attempting to simulate high-Reynolds-number rotary characteristics in subscale tests using boundary-layer trips alone or in combination with forebody strakes
Sign-in/Register to access full text options 
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.
