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Members of the Committee
Report of the Committee for the year 193132 1
Appendices to the Report
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aerofoil aeroplane aircraft airscrew thrust altitude control angle approximately axis blade body interference boundary layer Bristol Bulldog calculated cent chords run circuit component constant corresponding curves determined diameter direction disc distance drag coefficient ebonite effect engine equation experimental experiments Figure flow fluid foil form drag forward pusher ft./sec full scale given heat transfer helmet cowl incidence increase interference drag investigation length of run lift coefficient measured method nacelle National Physical Laboratory nickel strip observed obtained photographs plane plate plotted pusher position range rate of climb ratio represented resistance Reynolds number screw shown slipstream solution spinner spinning steady motion stream surface friction TABLE take-off tank temperature Tests with Nacelle theoretical torque total head Townend ring tractor position tube turbulence velocity vortex vortex ring vorticity Wagner's theory wake wind gradient wind tunnel wing zero