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System Analyses and Autopilot Design for Automatic Roll Stabilization of a Supersonic Pilotless Aircraft (1951)
NASA Technical Reports Server (NTRS) · leaf 27
ro ON NACA RM L51E07 Figure 2.- Typical airframe 0/5a frequency response graphical construction on semilog graph paper. —^ = 252* ^ = 0.6* Iv = 2.5; M = 2.5; altitude, 40,000 feet; L0 = i estimated value.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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