It is shown that, if sweepback angle is not more than 35° it is possible to make wing aeroisoclinic by introducing swept stringers.


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    Title :

    Some structural parameters for aero-isoclinic wing


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1952


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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