"A method is presented for calculating wing characteristics by lifting-line theory using nonlinear section lift data."@en
"The wing characteristics calculated from general nonlinear section lift data have been found to agree much closer with experimental data in the region of maximum lfit coefficient than those calculated on the assumption of linear section lift curves. The calculations are subject to the limitations of lifting-line theory and should not be expected to give accurate results for wings of low aspect ratio and large amounts of sweep."@en
"A method is presented for calculating wing characteristics by lifting-line theory using nonlinear section lift data. Material from various sources is combined with some original work into the single complete method described."@en
United States. National Advisory Committee for Aeronautics.
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