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NOVEMBER 1938 Number
Effect of Wing Twist upon Stresses Due to Bending H W Sibert
Desirable Qualities of Transport Airplanes from the Pilots Point of View
6 other sections not shown
Aero Digest aerodynamic Aeronautical Sciences Aeroplane aileron Aircraft Engineering airfoil airplane alloys altimeter altitude aluminum angle angle of attack application Aviation axis balloon bomber boundary layer calculated carburetor characteristics coefficient combustion compression constant corrosion Cruising speed curve cylinder described developed discussed drag effect equations equipment experimental factor flaps flight flow flying boat forces frequency fuel fuselage gear given Hispano-Suiza illus increase indicated Institute instrument Journal landing load material Maximum speed measured ment metal meters method monoplane obtained operation paper percent performance photographs pilot plane plate present pressure problem propeller radial radial engine radio range ratio reference Reynolds Number rivet Rolls-Royce Merlin shear shows single-seater stability steel stiffener stress structure supercharger tables tail take-off temperature tests tion torque tube turbulence valve velocity vertical surfaces vibration weight welding wind tunnel wing Wright Brothers