The Adaptive Compliant Trailing Edge (ACTE) project modified a Gulfstream III (GIII) aircraft with a new flexible flap that creates a seamless transition between the flap and the wing. As with any new modification, it is crucial to ensure that the aircraft will not become overstressed in flight. To test this, Star CCM a computational fluid dynamics (CFD) software program was used to calculate aerodynamic data for the aircraft at given flight conditions.


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    Titel :

    ACTE Wing Loads Analysis


    Beteiligte:
    Horn N. R. (Autor:in)

    Erscheinungsdatum :

    2015


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    ACTE Wing Loads Analysis

    Horn, Nicholas R. | NTRS | 2015


    Eurostar Acte II

    Fressoz, Marc / Grassart, Pascal / Poingt, Marie-Hélène et al. | IuD Bahn | 1998


    Wing Loads

    Lomax, Ted L. | AIAA | 1996


    Britische Zolltarif-Acte

    GWLB - Gottfried Wilhelm Leibniz Bibliothek | 1855