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aerodynamic aerofoil aeroplane aileron Air Ministry aircraft airspeed angle approximately axis B.Sc blades body Bristol Fighter buffeting calculated cent chord CN CN constant correction corresponding curve cylinder density diameter distance distribution drag coefficient effect elastic equation experiments fairing flight flow form drag frequency ft./sec full scale G. I. Taylor given gradient hinge incidence increase inertia interference interference drag investigation level speed lift lift coefficient maximum measured method motion National Physical Laboratory normal observed obtained oscillations pipe pitch airscrew plane plotted product of inertia range rate of climb ratio reduced Reynolds number ring rotation screen shown in Fig skin friction slipstream stiffness strut supercharge height supercharged engines surface Table tail tailplane tests theoretical thrust torque torsional Townend Ring tube turbulence V/nD values vanes variation velocity vortex wheel wind speed wind tunnel wing position wire zero