The lift, drag and pitching moment on five symmetrical slender-wing models with sharp edges and aspect ratios of 1.28 and 1.46 have been measured at low subsonic speed. Four of the models had a gothic planform and one a ...

To provide data for stressing purposes, measurements have been made of the effect of sideslip on the rolling moment on a 41.5-deg swept-back tailplane mounted at three heights on the fin of a one fifth scale model of a ...

An experimental investigation has been made of the subsonic lift, drag and longitudinal stability characteristics of models representing some alternative slender airbus configurations. For the same wing planform of aspect ...

In view of the possibility of trimming some swept-wing aircraft at incidences above the stall, there has been a desire to visualise the whole pattern of vortex sheets and separated flow starting from the stalling wing, and ...