Wind-tunnel test technique was evolved and data from preliminary test series were reduced to develop and to evaluate method; existing model was modified by slitting wing chordwise at seven spanwise stations leaving spar intact and attaching strain gages to measure wing bending moments; reduction method used avoids need to differentiate bending-moment variation by curve-fitting unknown span loading variation; data reduced are presented for typical test conditions.


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    Titel :

    Segmented wing test technique for obtaining spanwise load distributions


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:
    Wasson, H.R. (Autor:in) / Mehus, T.E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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