Page 17 - Pressure Vessel Design Manual
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4    Pressure Vessel Design Manual
                                                                  ,- Failure surface (yield surface boundary)
                         P
                              t O1
























                                           Figure 1-2.  Graph of  maximum shear stress theory.

         which  would  cause yielding  as  predcted  by  the  maximum   ASME Code, Section VIII, Division 2, and Section I11 use
         stress theory!                                        the  term  “stress  intensity,”  which  is  defined  as  twice  the
                                                               maximum  shear  stress.  Since the  shear  stress  is  compared
                                                               to one-half the yield stress only, “stress intensity” is used for
                Comparison of the Two Theories                 comparison  to  allowable  stresses  or  ultimate  stresses.  To
                                                               define  it  another  way, yieldmg begins when  the “stress in-
           Both theories are in agreement for uniaxial stress or when   tensity” exceeds the yield strength of the material.
         one of  the  principal  stresses  is  large  in  comparison  to  the   In the preceding example, the “stress intensity” would be
         others.  The  discrepancy  between  the  theories  is  greatest   equal to 04 - a,. And
         when both principal  stresses are numerically equal.
           For simple analysis upon which the thickness formulas for
         ASME Code, Section I or Section VIII, Division 1, are based,
         it  makes  little  difference  whether  the  maximum  stress   For a cylinder where  P = 300 psi,  R = 30 in., and t = .5 in.,
         theory or maximum shear stress theory is used. For example,   the two theories would compare as follows:
         according  to  the  maximum  stress  theory,  the  controlling
         stress governing the thickness of a cylinder is 04, circumfer-   Maximum stress theory
         ential  stress,  since  it  is  the  largest  of  the  three  principal
         stresses.  Accordmg  to  the  maximum  shear  stress  theory,
         the controlling stress would be one-half the algebraic differ-   o = a4 = PR/t  = 300(30)/.5  = 18,000 psi
         ence between the maximum and minimum stress:
                                                                 Maximum shear stress the0 y
           The maximum stress is the circumferential stress, a4
                                                                  a = PR/t + P = 300(30)/.5 + 300 = 18,300 psi
            04  = PR/t
                                                               Two points  are obvious from the foregoing:
         0  The minimum  stress is the radial stress, a,
            a, = -P                                              1. For  thin-walled  pressure  vessels, both  theories  yield
                                                                   approximately the same results.
         Therefore, the maximum shear stress is:                 2.  For thin-walled pressure  vessels the  radial stress is  so
                                                                   small in comparison to the other principal stresses that
                                                                   it can be ignored and a state of biaxial stress is assumed
                                                                   to exist.
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