Span load distribution for tapered wings with partial-span flaps (1937)
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rectangular wing having a 0.6-span constant- strength at every section along the span is equal to the chord split flap. The wing used was of Clark T section circulation T at that section. The lift per unit length of span is then with a 20-inch chord and a total span of 120 inches. Some of the… … 0 Percent semi span Percent semispan cb Fiqure 4.—Typical distributions of a -g and cj doe to a flap deflection. W=6; /S«i=1.0.) Figure 6 shows comparisons of computed and experi- any shape. The relations between r, c{, and ao are given by the equations mental values of AOL for various flap…
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