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1.4.2 The rod of rectangular section
                                                   Bending  in  two  planes
                                           and  torsion  rod  of  rectangular
                                           cross  section  (fig.  1.11)  there
                                           appear  normal  and  shear
                                           stresses,  their  diagrams  are
                                           shown  in  fig.  1.12.  Tangential
                                           stresses are acting in the plane
                                           of the cross-section and normal
                                           - normal to it.
                    Figure 1.11
                                                  Dangerous  may  be  one
                                           of the points 1, 2 or 3. At point

                                           1 normal stresses of bending in
          both planes reach extreme value and the tangent is zero. Stressed
          state is linear, and the condition of strength has the form
                                  M     M
                                              
                                  y    z     .                (1.26)
                            max
                                  W     W
                                    y     z
                                                    At  points  2  and  3
                                             there  act  normal  stresses  of
                                             bending         (   and
                                                               M  y    M  z
                                             accordingly) and the tangent
                                                  of  torsion.  Tangential
                                               M  x
                                             stresses  from  bending  are
                                             usually  neglected  due  to
                                             their  smallness  compared
                                             with  the  tangential  stresses
                                             from torsion. At these points
                                             the  stress  state  is  flat  and
                                             strength  assessment  should
                                             use  one  of  the  theories  of

                                             strength.  Recall  that  to
                     Figure 1.12             estimate  the  strength  of  the
                                             rod  of  plastic  material  the
          third  or  fourth  strength  theory  are  commonly  used,  but  if  the
          material is fragile - a theory Mora.
                  For example, the conditions for third strength theory (the
          theory of greatest shear stresses) are of the form:
                 – to the point 2

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