This report results from a contract tasking University of Manchester as follows: The contractor will investigate using a variable stiffness vertical tail attachment to control aeroelastic performance over a range of dynamic pressures. The contractor will (1) Develop an adaptive stiffness attachment for vertical tail aircraft; (2) Develop an analytical model of the attachment and predict aeroelastic performance; (3) Design build and test a vertical tail model with and without a rudder to demonstrate the concept and validate the theoretical predictions; and (4) Conduct wind tunnel testing at sub and supersonic Mach Numbers; and (5) Consider the extension of the design for full- size aircraft and to quantify the benefits.


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    Titel :

    Variable Stiffness Concept For Efficient Aircraft Vertical Tail Design


    Beteiligte:
    J. E. Cooper (Autor:in) / O. Sensburg (Autor:in) / M. Amprikidis (Autor:in)

    Erscheinungsdatum :

    2003


    Format / Umfang :

    30 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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