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.


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    Titel :

    Static Aeroelasticity in Combat Aircraft


    Erscheinungsdatum :

    1986


    Format / Umfang :

    44 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Static aeroelasticity in combat aircraft

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





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