TIONAL ADVISORY COMMITTEE FOR AERONAUTICS then apply a correction for the stagger corresponding , bn± bL to each angle of attack. Figure 4 gives the varia- 6 10 la a. a tion of mGO with stagger in terms of the value of ja(X) for zero stagger. Figure 5 gives the variation of m(a) with' stagger in… … _ ba + 6& ^ 6t7 - 6i ~SS~ Az~ Fiqube L—Values of p "(X). ±4 ±8° ±12' ±16° ±20° ±24° ±28° Sfogger, /3 Fiottbe 4.—X- 1.20 <o WO a 80 FlQUEE 2.—r (X) for -/S°—F (X) iOf+P". .60 edge) of the upper and lower wings. Stagger is posi- tive when the third point in the upper wing is ahead .40 of the lower…
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