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actuating tube aileron aileron hinge aircraft airscrew alloy aluminium angles of incidence angular velocity APPENDIX aspect ratio auxiliary aerofoil axes axis B.Sc balancing spring Brinell Bristol Fighter Aeroplane Broken Broken cent centre of pressure constant control column corrected corresponding crankshaft curves cylinder derivatives diagram diameter effect engine equation experiments fatigue limit fitted fracture full scale give given in Table increase inertia lateral control lift coefficient machine measured method motion movement obtained oscillation pilot planes pitch plates plotted rate of roll real roots rear link Reports and Memoranda rolling and yawing rudder servo servo flap shear stress shown in Fig shows sideslip slip direction SLOTS INTERCONNECTED slotted wing specimen speed spin spring hub Stability Derivatives stalled flight thorium torque torsiograms TORSIOGRAPH TESTS torsional trailing edge twin bands twinning planes unslotted values vibration wing tips wire zero