The report describes results obtained from applied loading of the wing surfaces of an F-102 aircraft.


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    Title :

    Model 8-82 Wing-Tip Deflection Test


    Contributors:
    R. J. Haney (author) / W. E. Wise (author)

    Publication date :

    1954


    Size :

    48 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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