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General Conditions for Ascertaining the Strength of Aircraft
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Aeronautical aeroplane aileron Aircraft Engineering airscrew angle applied approximately assumed auxiliary aerofoil axes beam bending moments biplane blade element blade width C.P. forward calculated cent centre of pressure centre section Chart chord coefficient compression contraflexure cross-section curves deflection diameter drag drag coefficient duralumin end load equations Factor required Feet flying boat formula fuselage given horizontal Horse-power Inches incidence inertia interference velocity lateral load length lift lift coefficient load factor main planes maximum Metres Millimetres modulus N.A.C.A. Report normal top speed panel pitch points of support Radians ratio rivet Royal Aeronautical Society screw shear force shear stress side load slipstream slot solidity spar standard radius strain energy strength structure strut tail plane taken tapered tensile tension tests thickness Three Moments tip speed tons/sq torque Torsion tube undercarriage vertical weight Welded wheel wing wires Young's modulus zero