A flight investigation of the reduction of aileron operating force by means of fixed tabs and differential linkage, with notes on linkage design (1938)
NASA Technical Reports Server (NTRS) · leaf 21
0 ~4 8 12 16 20 24 Stick deflection, leg. Figure 11.- Variation with stick position of the stun of the upward and downward deflections of the two ailerons on the standarl wing for the final linkage.
NASA Technical Reports Server (NTRS)
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