A series of low-speed wind tunnel tests of a Blended-Wing-Body tri-jet configuration to evaluate the low-speed static and dynamic stability and control characteristics over the full envelope of angle of attack and sideslip are summarized. These data were collected for use in simulation studies of the edge-of-the-envelope and potential out-of-control flight characteristics. Some selected results with lessons learned are presented.
Blended-Wing-Body Low-Speed Flight Dynamics: Summary of Ground Tests and Sample Results
47th AIAA Aerospace Sciences Meeting and Exhibit ; 2009 ; Orlando, FL, United States
05.01.2009
Aufsatz (Konferenz)
Keine Angabe
Englisch
Blended-Wing-Body Low-Speed Flight Dynamics: Summary of Ground Tests and Sample Results (Invited)
British Library Conference Proceedings | 2009
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