Maneuverability Investigation of an O3U-1 Observation Airplane (1934)
NASA Technical Reports Server (NTRS) · leaf 13
. The results obtained by this method were erratic, pos- where 0 is the angle of bank, given by the expression sibly because the airplane was traveling in its own wake. ^cos-^J (10) For the second method the data required from the steady turns were air speed and corresponding engine and Vi/V is the… … Time, seconds Longitudinal displacement, feet Longitudinal displacement, feet 0 400 800 1200 1600 400 800 1300 1600 < 600 200 8 £ - 400 0 < ft* Si -200 -200 .to -400 Figure 25.—Immelinan turn (OSU-l airplane). Figure 24— Half kick roll—lialf loop (OSU-l airplane). Radii calculated by this method…
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