A Method for the Determination of the Spanwise Load Distribution of a Flexible Swept Wing at Subsonic Speeds. Skoog, R. & Brown, H. Technical Report TN-2222, National Advisory Committee for Aeronautics, 1951.
bibtex   
@TechReport{Brown1951,
    author      = {R.B. Skoog and H.H. Brown},
    title       = {A Method for the Determination of the Spanwise Load Distribution of a Flexible Swept Wing at Subsonic Speeds},
    institution = {National Advisory Committee for Aeronautics},
    number      = {TN-2222},
    year        = {1951}
}

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