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The Design of Modern Steel Bridges - TEDI

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40 <strong>The</strong> <strong>Design</strong> <strong>of</strong> <strong>Modern</strong> <strong>Steel</strong> <strong>Bridges</strong><br />

parameters; for example, for the determination <strong>of</strong> yield stress British Standard<br />

BS 18[1] limits the rate <strong>of</strong> straining at the time <strong>of</strong> yielding to 0.0025 per<br />

second; when this cannot be achieved by direct control, the initial elastic<br />

stressing rate has to be controlled within the values stipulated for different<br />

testing machine stiffnesses.<br />

Within a zone <strong>of</strong>, say, 50 mm from a rolled edge, yield stress may be up to<br />

15% higher than in the remainder <strong>of</strong> a plate. Yield stress in the transverse direction<br />

may be approximately 21 2 % less than in the longitudinal direction <strong>of</strong> rolling.<br />

<strong>The</strong> yield stress (and also the tensile strength) varies with the chemical<br />

composition <strong>of</strong> the steel, the amount <strong>of</strong> mechanical working that the steel<br />

undergoes during the rolling process and the heat treatment and/or cold<br />

working applied after rolling. Thinner sections produced by an increased<br />

amount <strong>of</strong> rolling have higher yield stresses; even in one cross-section <strong>of</strong> a<br />

rolled section the thinner parts have higher yield stresses than the thicker parts.<br />

Heat treatment or cold working may remove the yield phenomenon.<br />

<strong>The</strong> stress–strain behaviour under compression is normally not determined<br />

by tests and is assumed to be identical to the tensile behaviour. In reality the<br />

compressive yield stress may be approximately 5% higher than the tensile<br />

yield stress. <strong>The</strong> state <strong>of</strong> stress at any point in a structural member may be a<br />

combination <strong>of</strong> normal stresses in orthogonal directions plus shear stresses in<br />

these planes. Several classical theories for yielding in three-dimensional stress<br />

states have been postulated; the theory that has been found most suitable for<br />

ductile material with similar strength in compression and tension is based on<br />

the maximum distortion energy and attributed variously to Huber, von Mises<br />

and Hencky. According to this theory, in a two-dimensional stress state yielding<br />

takes place when normal stresses s1 and s2 on the two orthogonal planes<br />

and shear stress t on these planes satisfy the following condition:<br />

s 2 1 þ s2 2<br />

s1s2 þ 3t 2 ¼ s 2 y<br />

where sy is the measured yield stress <strong>of</strong> the material. It may be noted that,<br />

according to this theory: (i) the<br />

pffiffiffi yield stress ty in pure shear, i.e. without any<br />

normal stresses, is equal to sy/ 3 and (ii) in the biaxial stress state, the normal<br />

stress in one direction may reach values higher than the measured uniaxial<br />

yield stress sy before yielding takes place; e.g. if s1 ¼ 2s2, yielding will not<br />

take place until s 1 reaches approximately 15% higher than the uniaxial yield<br />

stress <strong>of</strong> the material.<br />

<strong>The</strong> other elastic properties that influence the state <strong>of</strong> stress at any point are:<br />

(1) Young’s modulus E, which is in the range 200 to 210 kN/mm 2 .<br />

(2) <strong>The</strong> shear modulus or modulus <strong>of</strong> rigidity G, which is the ratio between<br />

shearing stress and shear strain and is in the range 77 to 80 kN/mm 2 .<br />

(3) Poisson’s ratio m, which is the ratio between lateral strain and longitudinal<br />

strain caused by a longitudinally applied stress and is usually<br />

taken as 0.3 for structural steel.

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