Handbook of Aeronautics: Structural principles and dataPitman, 1952 - Aeronautics |
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Common terms and phrases
acceleration aeroplane aileron alloy angle antisymmetrical applied area of plate average stress axial constraint stresses beam bending bending moment boom loads Bredt-Batho built-in calculated cantilever centroid coefficient combined compressive strength constant corresponding cross-section curved plates cylinder cylindrical tubes deflexions deformations diagonal tension diagram direct stress edge stress effect elastic end load engineers equation experimental factor factor of safety failing mode failing stress flange flat panels flat plates flexural axis flexural mode formulae four-boom tubes fuselage given gust half-wavelength inertia initial instability manoeuvring material maximum method modulus moment of inertia obtained pitching plane pure torsional ratio restraint ring rivets rotation Royal Aeronautical Society shear centre shear flows shear modulus shear stress simply-supported static stiffeners stiffness strength stress-system structure structure loading strut tangent area theory thickness torque torsion-bending torsional failure torsional mode transverse loads twist uprights values wavelength wing Young's modulus Z-section stringer