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THE ROYAL AERONAUTICAL SOCIETY
POWER UNITS FOR FUTURE AIRCRAFT
LOW DRAG AEROFOILS
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aero aerodynamic aeroelastic aerofoil aeroplane aileron airscrew all-wing alloy altitude applied beam bending bomber carrier cent civil coefficient combustion components compressibility compressor considerable critical Mach curve cylindrical tube deck deflection distribution drag effect efficiency elastic electrical equation equipment experience factor fighter fire flaps flight flow flutter flying four-boom Frederick Handley Page fuel function fuselage gas turbine gear given gust heat icing important increase installation jet engine layout lift lift coefficient limit Mach number machine maximum ment method necessary obtained operation paper pilot piston engine plane possible power plant pressure problem production propeller turbine range ratio reduced Royal Aeronautical Society Royal Aircraft Establishment Seafire secular equation shear shear stress shown speed Spitfire stall stress structure surface tailplane take-off tank temperature template tests thrust tion torque turbine engine undercarriage velocity vibration weight wing