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acceleration accuracy aeroplane age-hardening aileron Air Ministry air speed aircraft airscrew alloy aluminium anchor angles of incidence approximately axes axis B.Sc balance boundary Bristol Fighter calculated calibration cent centre of gravity chord coefficient control surface copper corrosion corrosion-fatigue cosh couple cracks curve cylinder deepened body diameter duralumin effect equation experiments feet per second flap given H. B. Irving heat-treatment hinge increase inertia length load machine manometer maximum measured method moments of inertia normal observed obtained Photograph pitching pitot pitot-static pitot-static tube pits plane Plate position pressure ratio recovery reduced resolved shear stress resolved stress rolling rotation rudder scale servo shear stress shown in Fig shows sideslip sinh slip bands slipstream slotted spars specimen spin stroboscope swirl symmetrical TABLE tail tailplane test-piece tests thickness torsional tube tunnel twin bands twinning values velocity white metal wing yawing zero