When studying stability of an aircraft, a quasi-steady aerodynamic model is often used. In this study, the results of a stability analysis of an unrestrained flexible forward swept wing aircraft using an unsteady aerodynamic formulation are compared to results obtained with a similar, but quasi-steady, aerodynamic formulation. In addition, the potential effects of wing tip stores on forward swept wing aircraft stability are explored. (Author)


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    Titel :

    Aeroelastic Stability of a Forward Swept Wing with Wing Tip Stores


    Beteiligte:
    W. G. Steele (Autor:in)

    Erscheinungsdatum :

    1982


    Format / Umfang :

    72 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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