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 -l.b° -.10 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… … a .degrees 71gare 11.- Connection between speed and control Tlgure 8,- Elevator moments. deflection In standard control system.
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