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262                                                    Part II Ultimate Strength


                 where M, is the fully-plastic moment, cry is the yield strength of the material and (SM), is
                 the plastic section modulus.
                 Frieze and Lin (1991) derived ultimate moment capacity as a function of normalized ultimate
                 strength of the compression flange using quadratic equation,
                                            /   \2
                      M,/M,=d,+d,L+d,  -                                             (13.32)
                                     CT
                                     OY
                 where
                  d,=-0.172,  d,= 1.548,  d,=-0.368,      for sagging

                  d,=0.003,  d, = 1.459,  d,=0.461,       for sagging
                 Mansour (1 997) reviewed the  above mentioned  empirical moment capacity equations and
                 compared them with test results.
                  Based  on  fully plastic  moment  interaction, Mansour and  Thayamballi (1980) derived the
                  following ultimate strength relation between vertical and horizontal moments,
                      m,+km;=1  if  lmyl<\m,\                                        (1 3.33)

                              =I
                      my +b: if  Imyl 2lm,l                                          (13.34)
                  where

                                                                                     (1 3.35)


                                (A+2A,)Z
                      k=                                                             (13.36)
                          16A,(A-A,)-4(AD  -AB)2
                      A= A,  +AB +2A,                                                (1 3.37)
                  and where
                      M,     = bending moment in vertical direction

                      My     =bending moment in horizontal direction
                      M,     = vertical ultimate collapse bending moment

                      M,     = horizontal ultimate collapse bending moment
                             = cross-sectional area of the deck including stiffeners
                      AD
                             = cross-sectional area of the bottom including stiffeners
                      AB
                      As     = cross-sectional area of one side including stiffeners
                  Mansour (1997) demonstrated the above equations fit well with finite element analysis results
                  for ultimate strength of hull girders under combined vertical and horizontal moments.
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