Impact and soft crash sizing simulations were performed using a finite-element global ground-aircraft model. Results are presented for the hard landing of a Mercure aircraft and the soft crash of a Falcon 900 aircraft. The data will be used as input in the dynamic and nonlinear modeling of hard crash problems for commuter-type aircraft such as the Falcon 10.


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    Title :

    Developpements et Perspectives dans le Domaine du Dimensionnement aux Impacts et au Crash aux AMD-BA (Avions Marcel Dassault-Breguet Aviation) (Developments and Perspectives at AMD-BA in the Field of Impact and Crash Sizing)


    Contributors:

    Publication date :

    1988


    Size :

    13 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English