Abstract This paper addresses the potential benefits due to a fully dynamic approach to determine the design loads of a mid-size business jet. The study is conducted by considering the fuselage midsection of the DAEDALOS aircraft model with landing impact conditions. The comparison is presented in terms of stress levels between the novel dynamic approach and the standard design practice based on the use of equivalent static loads. The results illustrate that a slight reduction of the load levels can be achieved, but careful modeling of the damping level is needed. Guidelines for an improved load definition are discussed, and suggestions for future research activities are provided.


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    Titel :

    Assessment of dynamic effects on aircraft design loads: The landing impact case


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    2015-06-15


    Format / Umfang :

    9 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Design Landing Loads Evaluation by Dynamic Simulation of Flexible Aircraft

    Ghiringhelli, G. L. / Boschetto, M. / North Atlantic Treaty Organization; Advisory Group for Aerospace Research and Development; Structures and Materials Panel | British Library Conference Proceedings | 1991