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Report of the Committee for the year 193132 1
Appendices to the Report
iii On the eddy system in the wake of fiat circular plates
1 other sections not shown
aerofoil aeroplane Air Ministry aircraft airscrew thrust altitude control angle approximately axis body drag boundary layer 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 holes incidence increase integration interference drag investigation length of run lift coefficient measured method nacelle National Physical Laboratory nickel strip nose observed obtained photographs plane plate plotted pusher position range rate of climb ratio represented resistance Reynolds number screw shown slipstream spinner steady motion stream surface friction TABLE take-off tank temperature theoretical thrust grading torque total head Townend ring tractor position tube turbulence velocity vortex vortex ring vorticity Wagner's theory wake wind gradient wind tunnel wing zero