Some recently declassified experimental data of rolling moment caused by sideslip measured at low speed on aeroelastic model of Douglas XA3D-1 airplane are presented; review of early simplified methods of analysis and correlation of one of methods with experimental results is shown; problem of estimating wing dihedral effect is reformulated in terms of structural and aerodynamic influence coefficients to utilize advances in lifting surface theory; experimental data and other examples indicate that aeroelastic change in dihedral effect at limit load factor can equal value measured on rigid models.


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    Titel :

    Dihedral effect of flexible wing


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Rodden, W.P. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Dihedral effect of a flexible wing

    RODDEN, W. P. | AIAA | 1974


    Dihedral Effect of a Flexible Wing

    WILLIAM P. RODDEN | AIAA | 1965




    Active dihedral control system for a torsionally flexible wing

    KENDALL GREG T / LISOSKI DEREK L / MORGAN WALTER R et al. | Europäisches Patentamt | 2017

    Freier Zugriff