Static longitudinal stability and longitudinal control of autogiro rotors (1938)
NASA Technical Reports Server (NTRS) · leaf 19
V.A.C.A. Technical Ifemorandian Uo. 879 TlgB. 3.5.8.9.10.11 … 5 10 IS 5 10 15 SO 0 a .degrees a .degrees Figure 3.- Helatlonshlp between angle 71gare 9.- Wing and tail moments of attcMk and air force for for standard control the described ezanople. system. .10 0 -.10 5 10 15 a, degrees -.20 Figure 10.- Total moments for 5 10 15 20 standard control a .degrees…
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