The Effect of Lateral Inclination of the Thrust Axis and of Sweepback of the Leading Edge of the Wing on Propulsive and Net Efficiencies of a Wing-Nacelle-Propeller Combination (1935)
NASA Technical Reports Server (NTRS) · leaf 8
Figs. 1,2 Figure 1.-Nacelle parallel to chord; wing -10° yaw. Figure a.-Haoelle 15° to chord; wing -20° yaw.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
