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 22
Fig. 12 N.A.C.A. Technical Note No, 653 A Tali deflection 0° O * » 10o + « « 20° … Percentage of maximum stick deflection i Figure 12.- Effect of tab deflection on maximum rolling velocity obtained with ailerons on standard wing with first modified linkage.
NASA Technical Reports Server (NTRS)
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