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advance ratio adverse yaw Aero aerofoil aeroplane ailerons aircraft aspect ratio B.Sc blade angle blade element blade setting calculated CD CD CD CD CN cent CM CM CM CM CN CN CM CN CN CN complete model compressibility Contra-Rotating Airscrews contra-rotating propellers critical Mach number curves diameter differential analyser downwash drag coefficient effect elevons engine equation experimental flaps flight tests flutter Forward Mach number fuselage high Mach numbers High Speed high-speed hinge I I I I I incidence increase lift coefficient low-speed maximum mean chord measured Meteor method nacelle ó ó ó ooooo ooooo ooooo Pitching moments pressure radius range reheat Reynolds number root root chord Royal Aircraft Establishment rudder scale model shown in Fig Spitfire stability strip theory tail tailplane thickness torque tunnel tests variation velocity weight Wind Tunnel yawing СЧ