System Analyses and Autopilot Design for Automatic Roll Stabilization of a Supersonic Pilotless Aircraft (1951)
NASA Technical Reports Server (NTRS) · leaf 29
28 NACA RM L51E0T … (b) Con^jarison of airframe ^/5a frequency responses for varying altitude, h0,000 feet; Ix = 2.5- aerodynamic damping. M = 2.5; Continued Figure 3
NASA Technical Reports Server (NTRS)
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