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Basic Definitions Note: For more detailed stress & strain
notes refer to webpage Stress & Strain Strain = Change in length (dL)over original length (L) e = dL / L Stress = Force (F) divided by Area withstanding Force (A) s = F / A Young's Modulus E = Stress ( s ) / Strain(e). This is a property of a material E = s / e Bending General Formula for Bending M / I = s / y = E / R W and w as used below for beam concentrated load, total load and uniform distributed load are assumed to be in units of force i.e. Newtons If they are provided in units of weight i.e kg then they should be converted into units of force by mutliplying by the gravity constant g (9.81) Simply Supported Beam . Concentrated Load ![]() Simply Supported Beam . Uniformly Distributed Load ![]() Cantilever . Concentrated Load ![]() Cantilever . Uniformly Distributed Load ![]() Fixed Beam . Concentrated Load ![]() Fixed Beam . Uniformly Distributed Load ![]() Torsion /Shear Poisson's Ratio = n = (lateral strain / primary strain ) Shear Modulus G = Shear Stress /Shear Strain G = t / g = E / (2 .( 1 + n )) General Formula for Torsion A shaft subject to a torque T having a polar moment of inertia J and a shear Modulus G will have a shear stress q at a radius r and an angular deflection q over a length L as calculated from the following formula. T / J = G . q / L = t / r Pressure Vessels - Thin Walled Cylinders For a thin walled cylinder subject to internal pressure P the circumferential
stress = p_c. This stress tends to stretch the cylinder along its length. This is also called the longitudinal stress. p_c = P . d / ( 4 . t ) For a thin walled cylinder subject to internal pressure P the tangential stress = p_t p_t = P . d / ( 2 . t ) The above two formulae are only valid if the ratio of thickness to dia is less than 1:20 Pressure Vessels - Thick Walled Cylinders
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Formulae_Index
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Last Updated 13/02/2010