Potential flow about arbitrary biplane wing sections (1937)
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ine segments cx and Cj given by transformation cos y\jp(\+ia)+p(\—ict)+2i}/ir] 14) are without "stagger" since the midpoint of each +i sin 7[p(X+ia)— p(\—ia)]=0 segment is located on the y axis (fig. 3 (b)). In order Elmploying the notation of equation (17) and the rela- to obtain further insight… … Angle of stagger, r .degrees quantities. In the general case of parallel segments Fiottbs 4.—Ohart presenting the angle of stagger i and the ratio of the periods of arbitrary stagger, there are given the three ratios against gap/ohord 0/e», and stagger/chord Sla In the special case of equal…
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