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322                                                         Chapter 5
         and the slenderness ratio, which is:





         the critical stress of Eq. (5.159) becomes:





         The critical  stress  is  plotted against the slenderness ratio in Fig. 5.57.





























                     Figure 5.57  Plot  of critical stress against the slenderness ratio

          The curve denoted by 1 is the graphical representation of the critical stress –
          slenderness  ratio of Eq.  (5.162), and  therefore the  elastic buckling is  only
          possible for values  lager than the value   which corresponds to the material
          proportionality limit.  For values  smaller than   which apply  to shorter
          columns – as the definition Eq. (5.161)  shows it, the  column  might  buckle
          inelastically  (the portions 2  or 3) or,  for very short columns, buckling is not
          even possible (the segment denoted by 4).  The curve 2  for instance represents
          the Engesser  model for  inelastic  buckling,  which  uses a  formula  similar to
          the one corresponding  to the  elastic  buckling of  Eq.  (5.162). The  only
          difference with this model is that Young’s modulus is no longer constant, and
          is  taken as either  the  tangent  or  secant  value from the  experimental  stress-
          strain curve,  or as  an  average combination of  the  two  values. Another
          solution is the Tetmajer-Jasinski  model, which  expresses a  linear relationship
          between the  critical  stress and  the  slenderness ratio.  While the  Engesser
          model works  better for metallic components,  the  Tetmajer-Jasinski  model is
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