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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    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1949


    Size :

    13 pages


    Remarks:

    Illus, Diagrs, Charts, Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :