Page 20 - Aircraft Stuctures for Engineering Student
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1.2 Notation for forces and stresses  5




























           Fig. 1.3  Values of stress on different planes in a uniform bar.


             However, to be strictly accurate, stress is not a vector quantity for, in addition to
           magnitude and direction, we must specify the plane on which the stress acts. Stress is
           therefore a tensor, its complete description depending on the two vectors of force and
           surface of action.


             1.2 Notation for forces and stresses

           It is usually convenient to refer the state of stress at a point in a body to an orthogonal
           set of axes Oxyz. In this case we cut the body by planes parallel to the direction of the
           axes. The resultant force SP acting at the point 0 on one of these planes may then be
           resolved into a normal component and two in-plane components as shown in Fig. 1.4,
           thereby producing  one component  of  direct  stress and  two  components  of  shear
           stress.
             The  direct stress component  is  specified by  reference to  the  plane  on which  it
           acts but the stress components require a specification of direction in addition to the
          plane. We  therefore allocate a single subscript to direct stress to denote the plane
           on which it  acts and two  subscripts to shear stress, the first specifying the  plane,
           the second direction. Thus in Fig.  1.4, the shear stress components are rzx and rzy
           acting on  the  z  plane and in the  x and y  directions respectively, while the direct
           stress component is oz.
            We may  now completely describe the state of  stress at a point  0 in a body by
           specifying components of shear and direct stress on the faces of an element of  side
           Sx, by, Sz,  formed at 0 by the cutting planes as indicated in Fig. 1.5.
             The  sides  of  the  element  are  infinitesimally small so  that  the  stresses may  be
           assumed to be  uniformly distributed over the surface of  each face. On each of  the
           opposite faces there will be, to a first simplification, equal but opposite stresses.
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