J. WEISSINGER method used to find lift-curve slope, spanwise center of pressure, aerodynamic center location, and span loading coefficients of untwisted and uncambered wings having wide range of plan forms; results presented in graphical form; methods for determining induced drag and approximate effects of compressibility.
Theoretical additional span loading characteristics of wings with arbitrary sweep, aspect ratio, and taper ratio
Nat Advisory Committee Aeronautics -- Tech Note
1947
17 pages
20 Supp plates, Bibliography
Article (Journal)
English
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