Investigation made to obtain experimental data on amount of gust load alleviation that might be expected as result of wings flexing under load; results indicated that unless adverse pitching motion could be eliminated or reduced, overall load reduction would be small; net reduction in bending moment, however, may be appreciable.


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    Titel :

    Gust-tunnel investigation of flexible-wing model with semichord line swept back 45°


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Reisert, T.D. (Autor:in)


    Erscheinungsdatum :

    1949


    Format / Umfang :

    13 pages


    Anmerkungen:

    Illus, Diagrs, Charts, Tables


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :