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iv Aircraft turning performance Part I S B Gates
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aerodynamic aerofoil aeroplane aileron aircraft airspeed angle approximately axis blades body buffeting calculated cent chord constant correction corresponding critical flutter speed 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 gauze given gradient hinge incidence increase interference interference drag investigation level speed lift lift coefficient maximum measured method moment of inertia motion National Physical Laboratory normal nozzle observed obtained oscillations pipe pitch airscrew plane plotted product of inertia range rate of climb ratio reduced Reynolds number ring rotation screw 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