Maneuverability Investigation of the F6C-3 Airplane with Special Flight Instruments (1932)
NASA Technical Reports Server (NTRS) · leaf 20
angent of the ratio of longitudinal second ^, respectively. A comparison of the flight and normal accelerometer readings was found to be 12°. paths for these three pull-ups (Figure 14) shows that Barrel rolls. -The results obtained in two barrel- vertical displacements varied in the same order as… … Time, seconds P'iGURE 22.—Second left spin m. p. h., and (hat of Figure 19 a left roll started at a Rudder maneuvers.—Two rudder maneuvers (Fig- speed of 140 m. p. h. There was also a dilTerence in ure 16) are included primarily for the purpose of indi- the control movements. The rudder and…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
