Wind-tunnel research comparing lateral control devices, particularly at high angles of attack III : ordinary ailerons rigged up 10 degrees when neutral (1933)
NASA Technical Reports Server (NTRS) · leaf 2
s great as, or greater than, the ment only with a maximum deflection of 60°. The adverse yawing moments with downward deflection, various relative displacements with the two differential from which it would seem that within reasonable movements are given in Table I, and linkage arrange- limits any… … Left down flight up Left down flight up Figure 2.—Yawing-moment ooeffldant doe to ailerons deflected individually FiouEE 3.—Yawing-moment coefficient due to ailerons deflected individually (body axes). Ailerons neutral 0" to wing chord (body axes). Ailerons natural up 10° from wing chord Aileron…
NASA Technical Reports Server (NTRS)
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