Page 16 - Pressure Vessel Design Manual
P. 16

Stresses in Pressure Vessels   3

          material  depends  only  on  the  numerical  magnitude  of  the   biaxial  state  of  stress  where  01  >  (~2, the  maximum  shear
          maximum  principal  or  normal  stress. Stresses  in the  other   stress will be  (al - (s2)/2.
          directions  are  disregarded.  Only  the  maximum  principal   Yielding will  occur when
          stress  must  be  determined  to  apply  this  criterion.  This
          theory  is  used  for biaxial states of  stress assumed in a thin-
          walled pressure vessel. As will be shown later it is unconser-
          vative in  some instances  and requires a higher safety factor   Both  ASME  Code,  Section  1'111,  Division  2  and  ASME
          for its use. While the maximum stress theory does accurately   Code, Section 111, utilize the maximum shear stress criterion.
          predict  failure  in brittle  materials, it is  not  always accurate   This theory closely approximates experimental  results and is
          for ductile materials.  Ductile  materials often fail along lines   also  easy  to  use.  This  theory  also  applies  to  triaxial  states
          45 to the applied force by shearing, long before the tensile   of  stress. In  a triaxial stress  state, this  theory predicts  that
          or compressive stresses are maximum.                  yielding will  occur whenever  one-half  the  algebraic  differ-
            This  theory  can  be  illustrated  graphically  for  the  four   ence between the maximum and minimum 5tress is equal to
          states of biaxial stress shown in Figure  1-1.        one-half the yield stress. Where c1 > a2 > 03, the maximum
            It can be seen that uniaxial tension or compression lies on   shear stress is (ul -
          tlir two axes. Inside the box (outer boundaries) is the elastic   Yielding will begin when
          range  of  the  material.  Yielding  is  predicted  for  stress
          combinations by the outer line.                       01 - 03 - F,
                                                                  2      2

                  Maximum Shear Stress Theory                   This  theory  is  illustrated  graphically  for  the  four  states  of
                                                                biaxial stress in Figure  1-2.
            This  theory  asserts  that  the  breakdown  of  material  de-   A  comparison  of  Figure  1-1 and  Figure  1-2 will  quickly
          pends only on the mdximum shear stress attained in an ele-   illustrate  the  major  differences  between  the  two  theories.
          ment.  It assumes that yielding starts in planes of maximum   Figure  1-2 predicts  yielding at  earlier  points  in  Quadrants
          shear stress. According to this theory, yielding will start at a   I1 and  IV.  For example, consider  point  B  of  Figure  1-2. It
          point when  the maximum  shear stress at that point  reaches   shows  ~2=(-)(~1;  therefore  the  shear  stress  is  equal  to
          one-half  of  the  the  uniaxial yield  strength,  F,.  Thus  for  a   c2 - ( -a1)/2,  which  equals  o2 + a1/2 or  one-half  the  stress



                                                                    r Safety factor boundary
                                                                       imposed by ASME Code
                        9                                      /                t O1
                                                       l+l.o
                                                        01


                                                       I





                                                                      +l.O

                                    -1.0                      I
                                                              I
                                              111      ____I    IV



                                                                  \
                                                       I -'.O
                                                       I                Failure surface (yield surface) boundary


          Figure 1-1.  Graph of  maximum stress theory. Quadrant I:  biaxial tension; Quadrant II: tension: Quadrant Ill:  biaxial compression; Quadrant IV:
          compression.
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