The prediction of aerodynamic loads is still a challenging engineering issue for military aircraft designers. Unsteadiness in the flow can lead to uncommanded motion and uncontrollable departure in flight testing.


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    Titel :

    Reduced Order Aerodynamic Loads Modeling of Maneuvering Aircraft


    Beteiligte:
    M. Ghoreyshi (Autor:in)

    Erscheinungsdatum :

    2012


    Format / Umfang :

    4 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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