Determination of Mean Camber Surfaces for Wings Having Uniform Chordwise Loading and Arbitrary Spanwise Loading in Subsonic Flow
S. Katzoff · M. Frances Faison · Hugh C. DuBose
Jan 1953 · National Advisory Committee for Aeronautics
Ebook
43
Pages
About this ebook
The field of a uniformly loaded wing in subsonic flow is discussed in terms of the acceleration potential. It is shown that, for the design of such wings, the slope of the mean camber surface at any point can be determined by a line integration around the wing boundary. By an additional line integration around the wing boundary, this method is extended to include the case where the local section lift varies with spanwise locatiion (the chordwise loading at every section still remaining uniform).
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