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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    ACTE Wing Loads Analysis


    Contributors:

    Conference:

    Student AIAA meeting ; 2015 ; Columbus, OH, United States


    Publication date :

    2015-08-04


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    ACTE Wing Loads Analysis

    Horn N. R. | NTIS | 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


    Telematique et multimedia: acte 2

    Automotive engineering | 2001