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                 118   Mechanical Engineering Design
                                3–18      Curved Beams in Bending            13

                                          The distribution of stress in a curved flexural member is determined by using the
                                          following assumptions:

                                          • The cross section has an axis of symmetry in the plane of bending.
                                          • Plane cross sections remain plane after bending.
                                          • The modulus of elasticity is the same in tension as in compression.

                                              We shall find that the neutral axis and the centroidal axis of a curved beam,
                                          unlike the axes of a straight beam, are not coincident and also that the stress does
                                          not vary linearly from the neutral axis. The notation shown in Fig. 3–34 is defined
                                          as follows:

                                                       r o = radius of outer fiber
                                                       r i = radius of inner fiber
                                                       h = depth of section
                                                       c o = distance from neutral axis to outer fiber
                                                       c i = distance from neutral axis to inner fiber
                                                       r n = radius of neutral axis
                                                       r c = radius of centroidal axis
                                                       e = distance from centroidal axis to neutral axis
                                                       M = bending moment; positive M decreases curvature

                                          Figure 3–34 shows that the neutral and centroidal axes are not coincident. The location
                                          of the neutral axis with respect to the center of curvature O is given by the equation
                                                                              A
                                                                                                           (3–63)
                                                                       r n =
                                                                               dA
                                                                               r


                  Figure 3–34                              a      b'                                 Centroidal
                                                                    b
                                                                                                       axis
                  Note that y is positive in the
                  direction toward the center of   c o
                  curvature, point O.                                               h                  e
                                                         y                                           y
                                                     c i                    M
                                                           d    c
                                           M
                                                                  c'             Neutral axis
                                                   r
                                                   o
                                                                                                          r
                                                                                                       r n  c
                                                         r i    d	                                   r
                                                             	      r n

                                                           O                                O



                                          13 For a complete development of the relations in this section, see Richard G. Budynas, Advanced Strength
                                          and Applied Stress Analysis, 2nd ed., Mcgraw-Hill, New York, 1999, pp. 309–317.
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