Page 106 - Pressure Vessel Design Manual
P. 106

General Design   87

        One can imagine a thin-walled cylinder loaded  axially to            Stiffening Rings
      the  maximum  extent  possible.  An  inward  circumferential
      load  does not  add any force longitudinally to  the cylinder;   Stiffening  rings,  either  internal  or  external,  should  be
      however, it increases the risk of buckling.           spaced at between  1 and 4 diameters. For vessels with stif-
                                                            fening rings, the length of the cylinder is determined by the
                        Safety Factor                       distance between the stiffening rings. This presupposes that
                                                            the stiffening rings are of adequate size and stiffness to resist
        The  allowable  buckling  stress  is  the  “critical  buckling   the  forces  imposed  on  them. The  design  of  the  stiffening
      stress”  multiplied  by  some  factor  of  safety.  The  safety   rings is not a part of this procedure.
      factor  for buckling  ranges  from  1.5:l to  3:l. In  addition,
      certain  upper  boundaries  are  specified,  such  as  one-half
      the yield strength.




       ALLOWABLE BUCKLING STRESS IN CYLINDRICAL SHELLS 114-201


                             Data

          A = metal cross-sectional area, in.  2
          B =ASME  Code allowable stress, psi
          C =end  connection  coefficient, use  1.0 for simply sup-
             ported and 2.0 for cantilevered
         C, = max allowable slenderness ration per AWWA D-100
         D,  = OD of cylinder, in.
          E = modulus of elasticity, psi
          e =tolerance  for peaking, in.
         FS = factor of safety                                                 Slenderness ratio, Ur
         Fy = minimum specified yield strength, psi         Figure 2-57.  Graph showing comparison of  column types with critical
         Fb = allowable longitudinal compressive stress, psi
          I = moment in inertia, in.  4
         L,  =length  at which critical stress is achieved, in.
           1 =tolerance  for banding, in.
         M = longitudinal bending moment, in.-lb
         P,  = critical external pressure buckling load, psi
         P,,  = critical buckling load, Ib
         Pi =internal  pressure, psi
         P,  = external pressure, psi
         R,  =vessel  outside radms, in.
          r = radius of gyration, in.
         T,  = factor  for  transition  between  elastic  and  inelastic
             buckling point per AWWA D-100                                             A
          t =wall  thickness, in.
         W =weight  of vessel above plane of consideration, lb
         a, =longitudinal  stress, psi
         a,., = critical stress, psi

      Allowable Stress, Fb                                                             -x-






                                                                                       7-
        For ASME Code vessels, Fb = Factor “B”
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