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.


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    Titel :

    Blended-Wing-Body Low-Speed Flight Dynamics: Summary of Ground Tests and Sample Results (Invited)


    Beteiligte:
    D. D. Vicroy (Autor:in)

    Erscheinungsdatum :

    2009


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Blended-Wing-Body Low-Speed Flight Dynamics: Summary of Ground Tests and Sample Results (Invited)

    Vicroy, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009



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    Carter, Melissa / Vicroy, Dan / Patel, Dharmendra | AIAA | 2009


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    Carter, M. / Vicroy, D. / Patel, D. et al. | British Library Conference Proceedings | 2009