Statical longitudinal stability of airplanes (1921)
NASA Technical Reports Server (NTRS) · leaf 18
dealing systematically with the effects of C. G. position and tail-plane setting. The curves for three different C. G. positions and a tail- plane angle of - 2,4° to the top longerons are plotted, both for open and for closed throttle, in figure 5. It will be observed that, as prophesied from the… … The effect of tail-plane setting is shown in figure 6, where the curves for three different settings with a constant C. G. position are given. The curves show that the stability is much better with the tail plane at -2.4° to the top longerons than with it- set at -1.4°, and that a further increase…
NASA Technical Reports Server (NTRS)
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