An aerodynamic optimization procedure developed to minimize the drag to lift ratio of an aircraft configuration: wing - body - tail, in accordance with engineering restrictions, is described. An algorithm developed to search a hypersurface with 18 dimensions, which define an aircraft configuration, is discussed. The results, when considered from the aerodynamic point of view, indicate the optimal configuration is one that combines a lifting fuselage with a canard.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    On a global aerodynamic optimization of a civil transport aircraft


    Beteiligte:
    Savu, G. (Autor:in) / Trifu, O. (Autor:in)


    Erscheinungsdatum :

    01.01.1991


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch






    The Global Aerodynamic Optimization of a Hypersonic Transport Aircraft

    Savu, G. / Trifu, O. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1993