This publication contains three papers presented to the Aeroelasticity Sub-Committee of the AGARD Structures and Materials Panel at its 60th Meeting. The papers show that static aeroelasticity is increasingly being considered as a primary design parameter, affecting as it does structural optimisation, vehicle aerodynamic stability control effectiveness and overall performance.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Static Aeroelasticity in Combat Aircraft


    Publication date :

    1986


    Size :

    44 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Static aeroelasticity in combat aircraft

    NATO, Advisory Group for Aerospace Research and Development | TIBKAT | 1986





    Static Aeroelasticity and Flutter

    Wright, Jan R. / Cooper, Jonathan E. | Wiley | 2014