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ROYAL AERONAUTICAL SOCIETY
ANONYMOUS the Tensile Strength of Metals W
Aircraft Welding L S Elzea XLVI Surgeoner J XLVI p 141
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Abstract available Aero Engine Aerodynamics Aeron aeroplane Aircraft airscrew Alloys altitude Aluminium angle applied Associate Fellow Avia Aviation axial axis beam bending blade Bomber Brinell Bristol Aero Engine Britain British calculated cent characteristic coefficient compression constant cross-section curve cylinder determined distribution dive drag effect equation fighter Flight flow Flugsport flying fuel Germany given Griffith Brewer Hammondsport hardness tests high speed horizontal increase Inter ITEM R.T.P. limit Lubrication Luftwissen machine material Mathematics maximum mechanical Metal method obtained operation Photograph pilot pitch plane possible pressure problem pyramidal diamond R.T.P. Translation radial ratio Research rotor Roy Fedden Royal Aeronautical Society shear stress Short Stirling steel structure strut Student supercharger surface taper temperature tensile strength theory TITLE AND JOURNAL turbine undercarriage velocity vertical weight Welding wheel Wilbur Wright wing loading